TABLE B-7 RESERVED …………………………………….……………... B-2 3 TABLE B-9 NTE PRICE LIST – STANDARD LAUNCH SERVICES FOR IDIQ MISSIONS………………………………………… B-5 TABLE B-10 NTE PRICE LIST – NON-STANDARD SERVICES FOR IDIQ MISSIONS………………………..……………….. B-6 TABLE C-2 RESERVED…………………………………………………….. C-28 TABLE C-3 RESERVED……………………………………………………. C-28 TABLE C-7 RESERVED ………………………….................…………….. C-3 C-8 C-3 TABLE C-9 RESERVED………………………………………………….... C-42 CAPABILITY for TBP Vehicle Configuration, Launch Site, and Ground Rules PAYMENT MISSION SUCCESS
SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS 1. REQUISITION NUMBER PAGE 1 OF 1 OFFEROR TO COMPLETE BLOCKS 12, 17, 23, 24 & 30 2. CONTRACT NO. 3. DATE 4. ORDER NUMBER 5. SOLICITATION NUMBER 6. SOLICITATION ISSUE DATE TBD RFP10-99-0021 Rev October 18,1999 7. FOR SOLICITATION INFORMATION CALL: a. NAME b. TELEPHONE NUMBER (No collect calls) 321-867- 8. OFFER DUE DATE/LOCAL TIME 9. ISSUED BY CODE OP-LS 10. THIS ACQUISITION IS 11. DELIVERY FOR FOB DESTINATION UNLESS NASA John F. Kennedy Space Center UNRESTRICTED BLOCK IS MARKED SEE SCHEDULE Procurement Office, Mail Code: OP-LS SET ASIDE: % FOR 12. OFFER ACCEPTANCE PERIOD Attn: , Room SMALL BUSINESS 180 Days from Date in Block 8 Kennedy Space Center, Florida 32899 SMALL DISADVANTAGED BUSINESS 13A. THIS CONTRACT IS A RATED ORDER 8(A) UNDER DPAS (15 CFR 700) 14. METHOD OF SOLICITATION 13B. RATING RFQ IFB RFP RFO SIZE STANDARD: 1000 DO-C9 15. DELIVER TO CODE OP-LS 16. ADMINISTERED BY CODE Same as Block 9. Same as Block 9. 17a. CONTRACTOR/ PPC/STATE OFFEROR CODE ( ) ( ) FACILITY CODE 18a. WILL BE MADE BY CODE NASA Shared Services Center (NSSC) Financial Management Division (FMD) – Accounts Payable Bldg 1111, C. Road Stennis Space Center, MS 39529 Email: Fax: 866-209-5415 TELEPHONE NO. 17b. CHECK IF REMITTANCE IS DIFFERENT AND PUT SUCH ADDRESS IN OFFER 18b. SUBMIT INVOICES TO ADDRESS SHOWN IN BLOCK 18a. UNLESS BLOCK BELOW IS CHECKED SEE ADDENDUM 19. ITEM NO. 20. SCHEDULE OF SUPPLIES/SERVICES 21. QUANTITY 22. UNIT 23. UNIT PRICE 24. AMOUNT NASA LAUNCH SERVICES IN ACCORDANCE WITH SECTION B, C AND D. (Attach Additional Sheets as Necessary) 25. ACCOUNTING AND APPROPRIATION DATA 26. TOTAL AWARD AMOUNT (For Govt. Use Only)
SECTION B STANDARD FORM 1449 CONTINUATION TABLE OF CONTENTS 1.1 Reserved……………………………………………….………………………. B-1 1.2 Reserved……………..………………………………………………………… B-1 1.3 Reserved……………………………………………………..………………… B-1 1.4 Reserved………………………………………………………………………. B-1 1.5 Special Task Assignment (Studies and Analyses)..………………………. B-1 1.6 IDIQ Launch Service Task Order (LSTO)………….………………………. B-2 1.7 NTE Prices - Standard Launch Services for IDIQ Missions……………… B-4 1.8 NTE Prices - Non-Standard Services for IDIQ Missions…………………. B-5 3.0 ……………..………………………….. B-6 3.1 ………………………………………………………………………. B-6 3.2 Reserved………………………………………………………………………. B- 3.3 Reserved………………………………………………………………………. B- LIST OF TABLES 1
24.0 DETERMINATION, INVESTIGATION, AND CORRECTIVE ACTIONS……………………………………………………... C-3 25.0 GOVERNMENT INSIGHT AND APPROVAL………………………………. C-3 27.0 LICENSES AND PERMITS FOR A LAUNCH SERVICE OPERATOR…. C-41 31.0 DOMESTIC SOURCE CRITERIA……………………………………………. C-47 33.0 FAR 52.212-3 OFFEROR REPRESENTATIONS AND CERTIFICATIONS – COMMERCIAL ITEMS ALT I …………………………………………..... C-50 34.0 FAR 52.212-5 CONTRACT TERMS AND CONDITIONS REQUIRED TO IMPLEMENT STATUTES OR EXECUTIVE ORDERS – COMMERCIAL ITEMS ……………………………………………………………..…………………….. C-5 35.0 RESERVED…………………………………………………………….……… C-5 36.0 LISTING OF CLAUSES INCORPORATED BY REFERENCE…………… C-5 37.0 FAR 52.252-2 CLAUSES INCORPORATED BY REFERENCE……..… C-5
Figure D1-5 Maximum Quasi-Steady Acceleration as a Function of Payload Separated Mass……………………………………………………….. D1-40 Figure D1-5A Maximum Thermal Environment During Ascent…………………… D1-40 Figure D1-6 Separating Secondary Payload Interface…………………………… D1-42 Figure D1-7 Non-Separating Secondary Payload Interface…………………….. D1-42 Figure D1-8 Through D1-13 RESERVED………………………………………………………….. Figure D2-1 Power -vs- Plus Count Time……………………………..…………… D2-39
Provide risk mitigation while utilizing commercial practices. Provide flexible manifesting policy that recognizes the national priorities of NASA missions. Provide a capability to optimize cost, schedule, and performance to satisfy mission objectives. Provide for clear Government visibility into program schedule, technical performance, and risk. Foster competition and create opportunities for new, emerging launch service providers. Promote partnering among customers, launch service providers, and the LSP to maximize flexibility and responsiveness to customers’ needs. 1.3 The Contractor shall comply with the requirements contained in the following documents. Document No. Revision Document Title Applicable Range Safety Requirements ISO 9001/ AS9100 KNPR 8715.3 LSP-PD-120.05 NPR 8715.6 NASA-STD-8719.9 2009 BASIC A (e.g., EWR-127-1, AFSPCMAN 91-710, International Organization of Standardization Aerospace Quality Management System KSC Safety Practices Procedural Requirements Launch Telemetry Requirements NASA Procedural Requirements for Limiting Orbital Debris NASA Safety Standard for Lifting Devices and Equipment ____________ The Contractor shall comply with the latest revisions of these documents. These documents apply to NASA property, personnel, software, and processes performed in NASA-owned facilities. The Contractor shall support NASA’s compliance with this document. DOCUMENTS
For missions with low tip-off requirements, switches may be required on either the payload or launch vehicle. Mounting details will be specified in the ICD. 8.0 Payload Environment The Contractor shall provide data for the maximum payload acoustic, vibration, shock, and acceleration, and thermal environment levels during launch and ascent. The maximum electromagnetic radiation levels encountered by the payload shall be depicted in Figure D1-3. The Contractor shall illustrate the pressure profiles and depressurization rates for each PLF in Figure D1-4. The maximum expected payload flight environments due to acoustics (50% fill), vibration, and shock shall be shown in Tables D1-K, D1-L, and D1-M, respectively. The maximum expected total acceleration (limit load factors), including uncertainty factors, shall be shown in Table D1-N (key dynamic events may be broken out as appropriate). The maximum expected sinusoidal vibrations at the base of the PA shall be shown in Table D1-O. The maximum quasi-steady acceleration as a function of payload separated mass shall be shown in Figure D1-5. The Contractor shall provide the maximum thermal environment during ascent for every launch component (i.e., upper stage, unblanketed skin, thermal/acoustic blankets, etc.) inside the fairing with a view factor to the payload in Figure D1-5A. TBP Figure D1-3: Maximum Electromagnetic Radiation Levels Encountered on Payload TBP Figure D1-4: PLF Pressure Profiles and Depressurization Rates TBP
Item Document Approval/ Review Initial Submittal Date Subsequent Submittal Date No. of Copies C4: Analysis C4-1* Performance and Guidance Accuracy Analysis (PGAA) Initial Submittal = Review, Subsequent Submittals = Approval ATP+ TBP L-12M; L-6M 3 C4-2* Final Mission Analysis (FMA) Approval Receipt of P/L Data + TBP A/R 3 C4-3* Payload/Expended Stage Separation Analysis Approval L-TBP L-TBP 3 C4-4* Payload Fairing Venting Analysis Approval Receipt of P/L Data + TBP A/R 3 C4-5* Payload Fairing Clearance Analysis Approval Receipt of P/L Model + TBP L-TBP; L-TBP 3 C4-6* Pre-Flight Controls and Stability Analysis Approval L-TBP A/R 3 C4-7* Coupled Dynamic Loads Analysis Approval Receipt of P/L Model + 3M L-15M L-26W 3 C4-8* Integrated Thermal Analysis Approval L-TBP A/R 3 C4-9* RF Link Analysis Approval L-12M A/R 3 C4-10* Payload/Launch Vehicle EMC, RF, and EED Compatibility Analysis Approval (B,C,D) L-12M (A & E) A/R in CDRL (B,C,D) L-3M (A & E) A/R in CDRL 3 C4-11* Mission Unique Software Approval Preliminary = L-TBP; Final = L-TBP A/R 3 C4-12* Quick Look Flight Report Review L+TBP N/A 3 C4-13* Final Flight Report Review L+TBP A/R 3 ___________________ * Required per mission TABLE D2-A: CDRL INDEX (Cont.) Item Document Approval/ Review Initial Submittal Date Subsequent Submittal Date No. of Copies C5: Engineering C5-1* Vehicle Data Package Review TBP As Changed 4 C5-2* Mission Unique Hardware Test Plan Approval ATP + TBP As Changed 4 C5-3* Mission Unique Hardware Test Report Review Test Completion + TBP As Changed 4 C5-4* Mission Specific Drawings Review As Generated per design review criteria, but no later As Changed 4
Performance capability, margins and reserves, including description of how performance reserve is calculated Sequence of events and tracking coverage Time history of trajectory from launch to targeted condition and end of mission maneuvers Launch vehicle summary weight statement Sources and magnitude for all dispersions used. If statistical dispersions are used, then the distribution method (e.g., normal, gaussian) shall be specified for each parameter Definition of all coordinate systems used Reference to the source(s) for all payload and launch vehicle inputs to this analysis (e.g., requirements, mass properties) Evaluation of compliance with applicable ICD requirements and constraints. (K) Launch windows determined by analysis (L) Input file CDRL DESCRIPTION Number: C4-2 FINAL MISSION ANALYSIS (FMA) DESCRIPTION/PURPOSE: This analysis is prepared based on payload requirements resulting from NASA review of the PGAA and contains information similar to that in the PGAA. This analysis supports pre-flight verification of compliance with mission requirements. DATA REQUIREMENTS: The FMA shall include, as a minimum: The nominal 5 or 6 Degree of Freedom (DOF) trajectory simulation for each targeted insertion condition utilizing actual weights and propulsion models (electronic format is preferred). All Data Requirements identified in PGAA Data Requirement Description.
9 L-05 Launch Vehicle Final Assembly and Test MSSAR Verification Coupled Dynamic Loads Cycle Contractor statement that final assembly and test of the Launch Vehicle is substantially completed and on schedule for shipment to launch site. Mission Specific System Acceptance Review (MSSAR) or equivalent complete and CDRL C1-1 has been submitted to NASA. Verification loads cycle complete and CDRL C4-7 has been approved by NASA. Approval of PGAA (L-6M) CDRL C4-1 10 L-02 Launch Vehicle Systems Readiness Review Obtain concurrence to erect L/V on pad, or to continue with L/V processing at the field site. Review includes mission overview, mission analysis, vehicle hardware and software, status on the factory buildup and launch site schedule. Mission Success Criteria & Determination and Methodology, CDRL C2-5 has been submitted and approved by NASA. 11 L Launch Launch event occurred and CDRL 4-12 has been delivered for review. 12 L+03 Mission Success Determination Final Flight Report completed and CDRL C4-13 has been submitted to NASA. 1 The “Program Event” and “Accomplishment Criteria” descriptions may be tailored to align with the contractor’s standard launch service process as long as the “Program Event” and “Accomplishment Criteria” descriptions remain substantially the same as is stated above. 2 If ATP is greater than L-30M the milestone date will be defined in the RLSP.