NAFCOM Global Input Parameters

Estimate Name:
\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_

Preparer's Name:
\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_

Revision Number:
\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_

Output Fiscal Year Dollars:
\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_

Launch Month:
\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_

Launch Year:
\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_

Database Normalization: \_\_\_\_ NASA \_\_\_\_ Air Force

Dollar Units: \_\_\_\_ Millions \_\_\_\_ Thousands

Learning Curve Type: \_\_\_\_ Unit (Crawford) \_\_\_\_ CUM Average
(Wright)

Decimal Places: \_\_\_\_ 0 \_\_\_\_ 1 \_\_\_\_ 2 \_\_\_\_ 3

Weight Display: \_\_\_\_ kgs \_\_\_\_ lbs

Year Type: \_\_\_\_ Fiscal \_\_\_\_ Calendar

Learning %: \_\_\_\_\_\_\_\_\_\_

Production Rate Per Year: \_\_\_\_\_\_\_\_\_\_

LRIP Step Down %: \_\_\_\_\_\_\_\_\_\_

Production Starts at Unit: \_\_\_\_\_\_\_\_\_\_

Rate %: \_\_\_\_\_\_\_\_\_\_

LRIP Quantity: \_\_\_\_\_\_\_\_\_\_

Stage/System Level Inputs

Production Quantity: \_\_\_\_\_\_\_\_\_\_

Functional Rates (FY01\$)

Engineering Labor Hourly Rate: \_\_\_\_\_\_\_\_\_\_

Manufacturing Labor Hourly Rate: \_\_\_\_\_\_\_\_\_\_

Other Labor Hourly Rate: \_\_\_\_\_\_\_\_\_\_

Overhead Rate: \_\_\_\_\_\_\_\_\_

G&A Rate: \_\_\_\_\_\_\_\_\_

Fee Percentage: \_\_\_\_\_\_\_\_\_\_

Program Support Percentage: \_\_\_\_\_\_\_\_\_\_

Contingency Percentage: \_\_\_\_\_\_\_\_\_\_

Vehicle Level Integration Percentage: \_\_\_\_\_\_\_\_\_\_

Notes:

\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_

ASE Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

GN&C/Attitude Control Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

# Computer? \_\_\_ Star Trackers? \_\_\_

**Horizon Sensors? \_\_\_ Gyros? \_\_\_**

**Sun Sensors? \_\_\_ Magnetometers? \_\_\_**

**Radar Altimiter? \_\_\_ Rendezvous Radar? \_\_\_**

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

### Stabilization Method: \_\_\_

**(1)** Spin Stabilized

**(2)** 3-Axis Stabilized

**(3)** Gravity Gradient

**(4)** Spin/Despin

GN&C/Attitude Control Subsystem Specific Inputs Cont.

# 

# Autonomy: \_\_\_\_

**(1)** Ground Control

**(2)** Sequencer/Timed Events

**(3)** Partially Autonomous

**(4)** Fully Autonomous

 

# Redundancy Rating: \_\_\_

**(1)** Not Redundant

**(2)** Partially Redundant

**(3)** Fully Redundant

# Funding Availability: \_\_\_

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

# Test Approach: \_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

Avionics Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

CC&DH Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

# Number of Transmitters: \_\_\_

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# 

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

# 

# Frequency Bands: \_\_\_

**(1)** 1 Band

**(2)** 2 - 3 Bands

**(3)** More Than 3 Bands  

**Redundancy Rating: \_\_\_**

**(1)** Not Redundant

**(2)** Partially Redundant

**(3)** Fully Redundant

CC&DH Subsystem Specific Inputs Cont.

# Funding Availability: \_\_\_

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

# Test Approach: \_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

Crew Accommodations Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

# Environment

**(1)** Launch Environment

**(2)** Orbiting Laboratory

**(3)** Extra Vehicular Environment

**(4)** Lunar or Planetary Surface

# Funding Availability: \_\_\_

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

Crew Accommodations Subsystem Specific Inputs Cont.

# 

# Test Approach: \_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

ECLS Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

**Crew Size: \_\_\_**

# Mission Duration (Days): \_\_\_

**Volume: \_\_\_**

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

# Environment: \_\_\_

**(1)** Orbiting Crew Module

**(2)** Launch Vehicle Attached Crew Module

**(3)** Launch Vehicle Crew Cabin

# Funding Availability: \_\_\_

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

## ECLS Subsystem Specific Inputs Cont.

# Test Approach: \_\_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

Electrical Power Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

**Output Power (watts): \_\_\_**

**Storage Capacity (amp/hrs): \_\_\_**

**Design Life (months): \_\_\_**

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

# Power Regulation: \_\_\_

**(1)**

Very Little Regulation

**(2)**

Moderate Regulation

**(3)** Highly Constrained Regulation

# 

# Funding Availability: \_\_\_

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

Electrical Power Subsystem Specific Inputs Cont.

# 

# Test Approach: \_\_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

Engines Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

Landing Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

# Funding Availability: \_\_\_

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

# Test Approach: \_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

Landing Subsystem Specific Inputs Cont.

# 

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

Miscellaneous Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

OMS Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

# Reusability: \_\_\_

**(1)** Expendable

**(2)** Reusable

 

**Environment: \_\_\_**

**(1)**

Launch Only

**(2)**

Launch and Orbit

# Funding Availability: \_\_\_

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

OMS Subsystem Specific Inputs Cont.

# 

# Test Approach: \_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

Propulsion Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

# Reusability: \_\_\_

**(1)**

Expendable

**(2)** Reusable

**Environment: \_\_\_**

**(1)**

LOX/RP

**(2)**

Launch Only

**(3)** Launch and Orbit

# Funding Availability: \_\_\_

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

Propulsion Subsystem Specific Inputs Cont.

# Test Approach: \_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

Range Safety Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

Reaction Control Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

**ISP (sec): \_\_\_**

**Thrust (lbs): \_\_\_**

**Propellant Weight (lbs): \_\_\_**

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

# Propellant: \_\_\_

**(1)** Hydrazine

**(2)**

Hydrogen Peroxide

**(3)** Nitrogen

# Funding Availability: \_\_\_

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

Reaction Control Subsystem Specific Inputs Cont.

# Test Approach: \_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

Recovery Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

**Funding Availability: \_\_\_**

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

# Test Approach: \_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

Recovery Subsystem Specific Inputs Cont.

# 

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

SRM Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

# Funding Availability: \_\_\_

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

# Test Approach: \_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

SRM Subsystem Specific Inputs Cont.

# 

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

# Retrorocket: \_\_

**(1)** No

**(2)** Yes

# 

# Upper Stage Only: \_\_

**(1)** Yes

**(2)** No

Structures Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

# Deployed: \_\_\_

**(1)** No Deployed Structure

**(2)** One Deployed Structure

**(3)** Multiple Deployed Structures

**(4)** Lunar or Planetary Surface

# 

# Funding Availability: \_\_\_

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

Structures Subsystem Specific Inputs Cont.

# 

# Test Approach: \_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

# Large Inert Structure?: \_\_

**(1)** Yes

**(2)** No

Thermal Control Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

# Design Life (months): \_\_\_

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

# External Cryogenic Storage Tank: \_\_\_

**(1)** Yes

**(2)**

No

# Funding Availability: \_\_\_

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

Thermal Control Subsystem Specific Inputs Cont.

# 

# Test Approach: \_\_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

# Louvers/Heaters: \_\_\_

**(1)** No Louvers

**(2)** Contains Louvers - Does not contain a Heater

**(3)** Contains both Louvers and Heaters

# Special Materials/Special Configuration: \_\_\_

**(1)** No

**(2)** Yes

Thrust Vector Control Subsystem Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Conventional Estimating

D&D Complexity Factor: \_\_\_\_\_\_\_\_

D&D Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

## Complexity Generator Estimating

**Manufacturing Methods: \_\_\_**

**0 to 12** \"Maximum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**13 to 37** \"Significant Use of Advanced Manufacturing Techniques Such
as JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**38 to 62** \"Moderate Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**63 to 87** \"Minimum Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**88 to 100** \"Limited Use of Advanced Manufacturing Techniques Such as
JIT Delivery, Bar Coding, Robotics, COTS, Outsourcing, etc.\"

**Engineering Management: \_\_\_**

**0 to 12** \"Minimum Design Changes With Design Team Making Maximum Use
of Highly Efficient \"Skunk Works\" Approach With IPTs, Rapid
Prototyping, Design to Cost, etc."

**13 to 37** \"Few Design Changes Using Highly Efficient \"Skunk Works\"
Approach With IPTs, Rapid Prototyping, Design to Cost, etc.\"

**38 to 62** \"Moderate Design Changes With Application of Advanced
Design Methods Including Concurrent Engineering, Tailored
Specifications, Minimum Reporting, etc.\"

**63 to 87** \"Dedicated Design Team Dependent on Some Technology
Advances Experiencing Significant Requirements Changes\"

**88 to 100** "Distributed Design Team Dependent Upon Major Technology
Advances Experiencing Frequent Major Requirements Changes\"

# New Design: \_\_\_

**0 to 10** \"Reflight of Existing Spacecraft, TRL-9\"

**11 to 21** \"Minor Modifications Not Requiring Re-Qualification,
TRL-9\"

**21 to 31** \"Minor Modifications Requiring Re-Qualification, TRL-9\"

**31 to 43** \"Moderate Modifications, TRL-9\"

**44 to 54** \"Moderate Modifications, TRL-8\"

**55 to 62** \"Significant Modifications, TRL-7\"

**63 to 72** \"Significant Modifications, TRL-6\"

**73 to 84** \"Based on a Previous Design, TRL-5\"

**85 to 95** \"Similar to a Previous Design, TRL-4\"

**96 to 100** \"New Design, TRL-3 thru TRL-1\"

**Funding Availability: \_\_\_**

**(1)** Funding is Assured -- No Delays

**(2)** Some Infrequent Delays Possible

**(3)** Funding is Constrained - Delays Likely

# Test Approach: \_\_

**(1)** Minimum Testing, Qualification Using Simulation and Analysis

**(2)** Moderate Testing, Qualification at Prototype/Protoflight Level

**(3)** Maximum Testing, Qualification at Component Level

Thrust Vector Control Subsystem Specific Inputs Cont.

# 

# Integration Complexity: \_\_\_

**(1)** Minimal Major Interfaces Involving Multiple Contractors/Centers

**(2)** Moderate Major Interfaces Involving Multiple Contractors/Centers

**(3)** Extensive Major Interfaces Involving Multiple
Contractors/Centers

# Pre-Development Study: \_\_

**(1)** 2 or More Study Contractors in Phase A&B - Greater than 9 Months
of Study

**(2)** One Study Contract - Between 9 and 18 Months of Study

**(3)** Less Than 9 Months of Pre-Phase C/D Study

System Integration Specific Inputs

System Integration Thruputs:

DDT&E IACO: \_\_\_\_\_\_\_

DDT&E STO: \_\_\_\_\_\_\_

DDT&E GSE/Tooling: \_\_\_\_\_\_\_

DDT&E M/E GSE: \_\_\_\_\_\_\_

DDT&E SEI: \_\_\_\_\_\_\_

DDT&E PM: \_\_\_\_\_\_\_

DDT&E LOOS: \_\_\_\_\_\_\_

Flight Unit IACO: \_\_\_\_\_\_\_

Flight Unit SEI: \_\_\_\_\_\_\_

Flight Unit PM: \_\_\_\_\_\_\_

Complexity/Heritage Factors:

DDT&E IACO: \_\_\_\_\_\_\_

DDT&E STO: \_\_\_\_\_\_\_

DDT&E GSE/Tooling: \_\_\_\_\_\_\_

DDT&E M/E GSE: \_\_\_\_\_\_\_

DDT&E SEI: \_\_\_\_\_\_\_

DDT&E PM: \_\_\_\_\_\_\_

DDT&E LOOS: \_\_\_\_\_\_\_

Flight Unit IACO: \_\_\_\_\_\_\_

Flight Unit SEI: \_\_\_\_\_\_\_

Flight Unit PM: \_\_\_\_\_\_\_

Scientific Instruments Specific Inputs

# Instrument Type: \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_

# Weight: \_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_\_\_**

Conventional Estimating

DDT&E Complexity Factor: \_\_\_\_\_\_\_\_

DDT&E Inheritance Factor: \_\_\_\_\_\_\_\_

Unit Complexity Factor: \_\_\_\_\_\_\_\_

Liquid Rocket Engine Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

Development Inputs

Design Process Improvement: \_\_\_

(Range: .1 - 1.0)

Certification Approach: \_\_\_\_

(Range: .1 -- 4.2)

Tooling Improvement Factor: \_\_\_\_

(Range: .1 -- 1.0)

Test Process Improvement: \_\_\_\_

(Range: .1 -- 1.0)

Tooling Availability Factor: \_\_\_\_

(Range: .1 -- 1.0)

Test Reduction Factor: \_\_\_\_

(Range: .5 -- 1.0)

Test Frequency/Month: \_\_\_\_

(Range: 10 - 30)

Production Inputs

Manufacturing Automation Level: \_\_\_\_

> Labor Intensive
>
> Semi Automated
>
> Automated w/Manual Testing
>
> Fully Automated

Manufacturing Process Maturity: \_\_\_\_

> New/Immature Process
>
> Similar/Modified Existing Process
>
> Existing/Mature Process

Design Maturity: \_\_\_\_

> Simple Modification
>
> Extensive Modification
>
> New Design
>
> New Product
>
> New Technology
>
> Advanced State of the Art

Design Process Maturity: \_\_\_\_

> Extensive experience with similar designs. Many experts/top talent
> leading the effort.
>
> Normal Experience, have completed similar type designs.
>
> Mixed Experience, some are familiar with the type design while others
> are new to the job.
>
> Unfamiliar with design, many are new to the job.

Liquid Rocket Engine Specific Inputs Cont.

Engine Cycle: \_\_\_\_

> GG or Exp. Or Tap-Off
>
> SC, Dual Preburner
>
> SC, Single Preburner
>
> Hybrid

Propellant Type: \_\_\_\_

> LOX/RP-1
>
> LOX/H2

Chamber Pressure (psia): \_\_\_\_

Reusability: \_\_\_\_

> Expendable
>
> Reusable

Producibility Factor: \_\_\_\_

(Range: .3 -- 1.0)

Thrust (Klbs): \_\_\_\_

Combined Cycle Propulsion Engine Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

**Fan Weight: \_\_\_\_**

**Exit Nozzle Weight: \_\_\_\_**

**MDC Fuel Injector Weight: \_\_\_\_**

**Ducts Weight: \_\_\_\_**

**MDC Turbopumps Weight: \_\_\_\_**

**Valves Weight: \_\_\_\_**

**Inlet Weight: \_\_\_\_**

**MDC Other Weight: \_\_\_**

**Number of Tests/Engine: \_\_\_\_**

> **More Complex/Less Mature**

##### Less Complex/More Mature

**Fuel Type: \_\_\_\_**

> **Hydrogen**
>
> **Hydrocarbon (JP, RP, etc)**
>
> **Other**

**Propellant Type: \_\_\_\_**

> **LOX/RP-1**
>
> **LOX/H2**

**Rocket Primary Chamber Pressure (psia): \_\_\_\_**

**Rocket Primary Vacuum Thrust (lbf): \_\_\_\_**

**Mach Number: \_\_\_\_**

**(Range: 4 -- 22)**

Turbojet Engine Specific Inputs

# Weight: \_\_\_\_\_\_\_\_\_\_\_\_\_

**STH Quantity: \_\_\_\_\_\_\_\_**

**% of Flight Unit: \_\_\_\_\_\_**

**Learning %: \_\_\_\_\_\_\_\_**

**QNHA: \_\_\_\_\_\_\_**

**Make %: \_\_\_\_\_\_\_**

**Contains the following New Design Components:**

> **High Pressure Turbine: \_\_\_\_**
>
> **Combustor: \_\_\_\_**
>
> **Controls and Accessories: \_\_\_\_**
>
> **Low Pressure Turbine: \_\_\_\_**
>
> **Afterburner: \_\_\_\_**
>
> **Nozzle: \_\_\_\_**
>
> **Compressor: \_\_\_\_**
>
> **Fan:\_\_\_\_**

**Maximum Thrust (lbs): \_\_\_\_\_\_\_**