Attachment 1 PM_TCE_FSO_RFI_Response_Matrix.xlsx
XLSX spreadsheet 11 KB Posted
- Solicitation number
- FA8819-RFI-SVUpperStage
About this file
This file is a response matrix template for a Request for Information (RFI) issued by Space Systems Command regarding orbit raising solutions for space vehicle upper stages. The RFI, numbered FA8819-RFI-SVUpperStage, seeks information on technologies and services that can minimize transfer time from Geosynchronous Transfer Orbit (GTO) to Geosynchronous Orbit (GEO), enabling rapid satellite placement while leveraging commercially available launch services to Low Earth Orbit (LEO) and GTO. The government seeks to evaluate emerging orbit raising systems for potential integration into its hybrid launch vehicle transport system as part of its Orbital Warfare and Space Domain Awareness missions.
The response matrix template captures essential vendor information across four primary categories: company details (name, CAGE code, DUNS, point of contact), technical capabilities (product name/model, throughput capacity, mass, electrical and mechanical interface control documents, GTO-GEO capacity, SWaP parameters, environmental compliance, and Technology/Manufacturing Readiness Levels), business information (rough order of magnitude pricing for single units and quantities of 10 and 20, production lead time, warranty terms, and intellectual property considerations), and supporting documentation (datasheets, brochures, and relevant test reports or field data). Respondents are required to provide comprehensive technical specifications that demonstrate their orbit raising solution's capability to minimize GTO-to-GEO transfer time while meeting government mission requirements.
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Text version
Orbit Raising Response Matrix
| Category | Parameter | Industry Response |
| Company Information | Company Name | |
| Company Information | CAGE Code / DUNS | |
| Company Information | Point of Contact (Name, Email, Phone) | |
| Technical Capabilities | Product Name / Model | |
| Technical Capabilities | Maximum Throughput (Orbit raising units/year) | |
| Technical Capabilities | Mass (kg) | |
| Technical Capabilities | Electrical ICD (attach, if available) | |
| Technical Capabilities | Mechanical ICD (attach, if available) | |
| Technical Capabilities | GTO - GEO orbit raising max capacity (kg) | |
| Technical Capabilities | SWaP (Weight, Power Requirements) | |
| Technical Capabilities | Environmental Compliance Standards | |
| Technical Capabilities | Technology Readiness Level (TRL) | |
| Technical Capabilities | Manufacturing Readiness Level (MRL) | |
| Business Information | ROM Cost – Single Unit | |
| Business Information | ROM Cost – Qty 10 | |
| Business Information | ROM Cost – Qty 20 | |
| Business Information | Production Lead Time (months) | |
| Business Information | Warranty Terms | |
| Business Information | Intellectual Property / Licensing Considerations | |
| Additional Information | Attach Datasheets / Brochures | |
| Additional Information | Provide Relevant Test Reports or Field Data |
File details come from the government source that posted it. Updated .