# Presentation: 844794

## HoneywellMobile Range Technology

**May 17, 2007**

## Range Safety System Architecture

**Range Safety System Architecture**

**Vehicle Position & Status Telemetry (downlink)**
**Command Destruct (uplink)**

**Two Mobile**
**5.4m Diameter**
**S-Band Tracking **
**Antennas**

**GPS-INS Tracking Unit (GITU)**
**mounted ****on the missile **

**Mobile Operations Center**
**Telemetry ingest**
**Data Processing**
**Range Safety Display**
**Command Destruct**

**Omni-Directional UHF**
**Command Destruct Antennas**

**Ground System Tracks Two **
**Independent Data Sources:**
**GITU (INS, GPS, & GPS-INS)**
**LV Telemetered Inertial Guidance**

**GPS Satellite**
**Constellation**

**Range Safety (EWR-127)**
**Telemetry, Tracking and Comm.**
**Classified and Unclassified Data Handling**
**Mobility**
**Transportable over Land, Sea, or Air**

**Notes:**
Effort begun in 1998
Address range concerns and requirements
Aging infrastructure – difficult and costly to maintain
More launches – federal and commercial launch ranges
- Mobility to cover wider trajectory range
- Rapidly reconfigurable
Incorporate metric GPS tracking
Deployment for military circumstances

## Mobile Range Safety and Telemetry System

**The Mobile Range Safety and Telemetry System**
**One mobile operations center**
**Two mobile antenna platforms with mobile power systems**
**Mobile range tracking and flight safety system **
**Augments the capabilities of existing launch ranges or**
**Acts as a completely self-contained range safety system**
**Receives and processes launch vehicle telemetry data**
**Generates displays used to verify that the LV remains in its predefined flight corridor **
**If the LV breaks the boundaries of that corridor**
**Flight Safety Officer can generate and transmit the appropriate command signal to terminate the flight.**
**Two redundant strings of processing equipment **
**Meets the high reliability and single fault tolerance requirements for safety-critical applications**

## Requirements Derivation and Management

**EWR 127-1**

**GPS Metric Tracking**
**Working Group**

**IRIG**
**Standards**

**RCC GPS Metric Tracking**
**Implementation Guidelines**

**System**
**Performance**
**Specification**

**Systems and **
**Subsystems Specification**

** ****Requirements Analysis**
** ****Requirements Derivation**
** ****Requirements Allocation **
** ****Verification Management**
** ****Automated Requirements ****   Management**

**Range**
**Presentations and**
**Discussions**

**Review with range safety community**

**45 SW RSOR Command Destruct System**

**30 SW WRR 127-9**

**FAA NPRM**

**Notes:**
Requirements from various sources – Range, working groups, IRIG....
Generate and flow down requirements
Review and agree on req’ts
Using DOORS req’ts management tool
Develop functional and operational req’ts

## Mobile User Telemetry System

**Up to 24 Telemetry channels **
**Data rates 10 Kbps – 20 Mbps**
**Pre-D recording**
**Post-D recording**
**PCM/FM, PCM/FM/FM, BPSK, **
**   ****A-QPSK, SOQPSK, Multi-H CPM**
**Growth capability designed in**

**Integrates with any L/S-band antenna system**
**150 Mbps Fiber Mux/Demux**
**Road/Sea/Air transportable**
**Supports Classified or Unclassified operations**

**Additional rack spaces available for external “User” equipment**
**Data archived and passed to users in real-time **

## Alaska Range Safety & Telemetry Systems

**Alaska Range Safety & Telemetry Systems**

*Honeywell’s integrated systems provide a complete range instrumentation solution*

**Kodiak Launch Complex**

**Cordova Launch Annex**

**Notes:**
In Alaska, Honeywell’s integrated systems provide a complete range instrumentation solution that is on the verge of being accepted as the prime and only system
Our systems in Alaska are located at
Kodiak Launch Complex
Off-axis/downrange sites Cordova Annex (King Salmon Annex)
At Kodiak, we have an RSTS and MTS. These are located at the instrumentation field (point to). The launch site is behind the photographer.
At Cordova, we also have an RSTS and MTS
Our last launch was the Missile Defense Agency STARS vehicle on February 24, 2006 and 
2-3 additional launches are planned for this year. 
For the next launch, the RSTS telemetry system is Prime, the Command Destruct System is hot backup. 
A successful mission will complete the acceptance program  to be Prime for subsequent launches from Kodiak
We support AADC with system sustainment, upgrades and mission operations.
Our customer has prepared a video to promote the Kodiak Launch Complex and I will show a portion of this that explains the uniqueness of KLC and describes our RSTS.

## Relocatable C3 for Gulf Ranges

**Testing and Training**
**Distributed environment for testing and training with net-centric weapons**
**Interoperable southeast range infrastructure (FL, GA, SC)**
**Support for large scale simulations**
**Enabling technology for Eglin as well as Central Test and Evaluation Investment Program (CTEIP)**

**Solution**
**Mobile element with remote / local control and monitoring**
**SATCOM integrated with classified joint tactical data links**
**Interoperable with Gulf ranges visualization environment for testing and training**
**Relocatable and scalable to southeast range infrastructure **

**Notes:**
Our Gulf Ranges customers from Florida to South Carolina need an improved testing and training environment

It should be:
Distributed range environment accommodating net-centric weapons (graphic)
Interoperable with southeast Ranges infrastructure
Able to support joint large scale simulations and exercises

Our solution:
Relocatable element as a key-node in the net-centric infrastructure (graphic)
SATCOM integrated with joint tactical data links
Interoperability with Gulf Ranges and visualization environment
Relocatable element has local / remote control / monitoring
Scalable platform for future growth to accommodate additional tactical data links and functions (SADL, Blue Force Tracking, ...)

## Relocatable C3 Platform

- Command Center Console, Storage, and Safe

- Rack Bay showing 1 of 3 racks and the power controls

- Platform with Omni Antenna

**Notes:**
Delivered relocatable platform
EMI racks from outside vendor – secure ops
Classified SATCOM -Inmarsat
Integrated on vibration platform

## Mobile Communications ConOps

**Private Cellular Network**
**Telephone Services**
**Streaming Video**
**Video Teleconferencing**
**Mast mounted camera**

**Land Mobile Radios**
**Handsets**
**Radio cross-banding**
**to Civil and Military **

**Virtual Private Network completed**
**by satellite link provides “encrypted tunnel”**

**Broadcast DTV**

**Ku band****High Rate Data**

**InfraLynx Truck**

**Command & Control**

**Wireless Internet**
**Power**

**InfraLynx SUV**

***Police***

***National Guard***

**Notes:**
Describe comm links

Explain simulated
	Civil radio cross banding
	Cellular network not included in this prototype

## First Responder/Command Post

**Communications**
**SATCOM for voice, data and video communications**
**Classified Video conferencing**
**Land Mobile Radios**
**Radio cross-banding for communicating with Civil authorities**
**Type 1 and/or AES encryption**
**Other**
**Conference room for 5 persons**
**Inside console for 2 persons**
**Mast mounted pan-tilt-zoom camera**
**Weather station**
**Power, telephone and data for up to 48 external users**
**Power generator with fuel for 24-hr**
**Safety**
**Low CG (Low mounting of generator, rack gear, batteries, etc.)**
**Wide Vehicle Track**
**Antilock Braking System**
**Drivability**
**Supports up to a 2.4 meter dish**
**Automatic transmission**
**GVWR < 40,000 lb **

## Response Vehicle, Team Vehicle 

**Ford F-550 Crew Cab XL**

**Freightliner M2 chassis**

**Consequence Management Team Vehicle**

**MIRV Body in Build**

**Major Incident Response Vehicle**

**Floorplan**

**Notes:**
MIRV and CMTV presently in build
Worked extensively with customers to define functional and operational needs.
Conference room
Classified SATCOM and VTC

## Summary

**Range safety / launch vehicle tracking and telemetry systems**
**Provide full range tracking and destruct capabilities**
**Augment capabilities of existing range**
**Integrate with existing infrastructure**
**Classified data handling**
**Mobile communication systems**
**Integrate communications for emergency response, first responders**
**On-site command post**
**Classified operations**
**Capabilities**
**System concept development**
**System requirements definition**
**Detail design analyses + trade studies + documentation**
**Subsystem procurement and supplier management**
**System integration and test**

## HoneywellMobile Range Technology

**May 17, 2007**

## HoneywellMobile Range Technology

**Backup**

## BMRST System Features

**Entire System Fits on Single C-17 Load**

**Displays Provide Mission Flight Safety Officers with Information for Range Safety Decisions**

- Rack 8

- Rack 9

- Rack 12 / 13
- Above Generator

- Rack 14 / 15
- Above Generator

**MFCO**

** ****Sr MFCO**

**TSO**

**CSO**

**SC**

- Rack 10

- Rack 11

**Cmdr**

**Notes:**
The BMRST system is designed to augment existing ranges and be deployed as a stand alone range safety system
To meet our customer transportability requirement, the Mobile Command Center, two antennas, power generators and a tow vehicle are carried in a single C-17 aircraft
The Mission Command Center is operated by 3 persons and a mission commander. 
Range safety responsibility rests with 2 Mission Flight Control officers (graphic)
The key personnel are:
System Controller – responsible for overall system configuration, checkout, and performance
Telemetry Systems Operator – responsible for antenna tracking and telemetry signal quality
Command Systems Operator – responsible for performance of the command destruct system

The mission commander implements pre-launch checkout, mission procedures  during the mission, and is responsible for communications with the Range

## Mobile Operations Center - Interior View

**Mobile Operations Center**** - Interior View**

- Telemetry Operator System  Console

- Command System Operator  Console

- MFCO Panel

## BMRST Deployments

**WSMR - Multiple Missions**

**Kodiak Launch Complex**
**QRLV-I and QRLV-II**

**Eastern Range – Atlas II**

**Space Shuttle STS-109**

**Notes:**
BMRST has been deployed in shadow mode for several launches 
Depicted here are:
Quick Reaction Launch Vehicles 1 and 2 from Kodiak Launch Complex 2001 & 2002
White Sands Missile Range – multiple missions conducted over a 6 week period 2003
Eastern Range – Atlas II 2004 & 2005
Space Shuttle 2002 
Later we will look at the BMRST systems deployed in Alaska.

## BMRST - Summary Capabilities

**Mobile on Single C-17 Load**
**Identical B2 and B3 Systems Available**
**Quickly Deployable**
**1-2 Day Set-Up Required**
**Minimal Footprint/Logistics Required**
**Shore Power/Generators/Battery Back-up**
**Very Flexible Interface Capability**
**Fully Capable Range Safety and Telemetry System**
**IRIG and Secure Tones**
**Up to 8 Channels of TM Processing**

**Notes:**
4 functional upgrades
Remote Command Destruct System
SATCOM interface
Data encryption / decryption
FIRST 3 BUILD CAPABILITIES TO PERFORM DOWN RANGE COMMAND DESTRUCT (FOR EXAMPLE  AT ANTIGUA)
4th is the Integration of customer furnished GRIDS Mission Flight Control Officer displays

Future upgrades will add telemetry capability and Eastern Range unique interfaces

## Mobile Telemetry System (MTS)

**Completed System Acceptance Test March 10, 2006**
**11 months after contract award**
**Shipped to Kodiak and Cordova in Alaska**
**Completed MTS / Range integrated system test on May 8, 2006**

## AADC Range Safety System Certification Status

**RSTS Formal Certification Process Completing 2006**
**PRST Leading Process**
**Multiple Test Phases**
**Detailed Performance Analyses**
**Operational Evaluation July 2005**
**3 Formal Shadow Missions**
**3 Formal Shadow Missions**
**IFT-13C Completed 2004**
**IFT-14 Completed 2005 **
**FT01-4 Completed Feb 2006**
- Full shadow with command destruct
**FTG-02 Completed Sept 2006**
- Full shadow with command destruct
**FTG-03 ILC Summer 2007**
- Full shadow with command destruct
**FTG-04 ILC Fall 2007**
- Primary range safety

## InfraLynx Security Vehicles

**Strategic Convoy Security**
**Secure voice, video and data communications between convoy vehicles and the Space Wing**
**Information and displays for situational awareness, command and control**
**Radio interoperability with civil and other authorities**

**Solution**
**Apply InfraLynx technologies from NRL**
**SATCOM integrated with joint tactical data links**
**Cross-banding military and public radios**
**Secure videoconferencing and telephone service**
**Common operational picture software**

**Incident Response**

**Consequence Management**

**Notes:**
Our Space Wing customers need to improve strategic convoy security

Current communications need to be improved:
Secure voice, video and data
Comm between vehicles and the Space Wing
Improved situational awareness
Interoperability with civil and other authorities

Our solution:
InfraLynx technologies from NRL and H-TSI
SATCOM integrated with joint tactical data links
Radio cross-banding
Secure telephone and videoconferencing
Common operational picture software
Two mobile platform types