Attachment 4-4 - Problem Statement 2.pdf
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- Attached to
- SSC/AATS SAFS 2. 1 Federal contract opportunity
- Solicitation number
- FA881124RB003
About this file
The provided document is an Attachment 4-4 - Problem Statement 2 for a Fair Opportunity Proposal Request (FOPR) under Solicitation FA8811-24-R-B003 for the Space Systems Command (SSC) Assured Access to Space (AATS) SAFS 2.1 Advisory and Assistance Services (A&AS) contract.
The document outlines a problem statement that requires the offeror to demonstrate their understanding of the Performance Work Statement (PWS) requirements by producing a Space Force Program Office Estimate. The estimate is for a fully burdened commercial launch vehicle required for a National Security Space (NSS) mission in Low Earth Orbit (LEO). Offerors are to consider current commercial launch providers that can develop the vehicle with minimal Government Mission Assurance. The estimate is for one mission launching from Cape Canaveral, with a payload weight of 15,000 lbs Mass to Orbit (MTO) in a 500 nautical mile circular orbit at 63.4° inclination. The launch vehicle is to be procured in Fiscal Year 2025, with a target launch in Fiscal Year 2027. The cost estimate shall be reported at the mean, and the response is to be provided as a standalone Microsoft Excel workbook with detailed documentation, sources, and risk parameters.
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Text version
Fair Opportunity Proposal Request (FOPR)
(FA8811-24-R-B003)
SSC/AATS
Attachment 4-4 Problem Statement #2
Problem Statement. You shall demonstrate your understanding of Section 3.2 of the PWS requirements by producing a Space Force Program Office Estimate that provides accurate calculations, insightful analysis and adequate documentation using the following parameters:
II. Estimate #2
1. Estimate Description: This NSSL risk-adjusted estimate is for a fully burdened commercial launch vehicle required for a NSS mission in LEO orbit. Consider companies currently in the market that would be able to develop this vehicle with minimum Government Mission Assurance. This estimate is for one mission launching from Cape Canaveral.
2. Input guidelines:
a. Utilize commercial launch providers
d. Consider expendable or re-usable options
c. Minimal Government Mission Assurance
d. Payload weight of 15,000 lbs Mass to Orbit (MTO), 500 nautical miles in a circular orbit at 63.4’ inclination
e. Launch vehicle procured in FY25, with a target launch in FY27
3. Cost Estimate shall be reported at the mean
4. Provide your response as a separate standalone Microsoft Excel workbook. The workbook shall be fully self-contained with no data links outside of the workbook. Linking cells to other tabs within the workbook is acceptable.
Include your source ACEIT file containing your model if used. Submit your estimate in electronic format only using the following guidelines:
a. Leave all formulas intact
b. Document your sources
c. Fully explain any Cost Estimating Relationships (CERs)
d. Provide Ground Rules & Assumptions as part of your hardcopy proposal
e. Provide risk parameters and justification
f. Provide an estimate for Other Government Costs (OGC)
g. Do not embed macros
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