ATT 02_DRAFT_HTRO_Self-Score Matrix_22 Oct 2025.xlsx
XLSX spreadsheet 18 KB Posted
- Attached to
- Andromeda Draft RFP
- Solicitation number
- FA881926RB001
About this file
This file is a draft self-scoring matrix for the Andromeda Indefinite Delivery Indefinite Quantity (IDIQ) solicitation (FA881926RB001) issued by the Department of the Air Force Space Command Space and Missile Systems Center. The matrix provides a detailed evaluation framework with three critical scoring factors for potential offerors: (1) Prime/Lead Integration of a Geosynchronous Earth Orbit (GEO) Space Vehicle, (2) Prime/Lead Integration of a Space-Based Electro-Optical System producing Space Domain Awareness resolved image data, and (3) Prime/Lead Integration of a Space Vehicle capable of Rendezvous and Proximity Operations (RPO).
The scoring matrix is binary, with offerors required to demonstrate capability in each factor through space vehicle projects launched within the last 5 years or scheduled for launch within the next 24 months. Each factor has specific technical requirements, such as GEO altitude specifications, intelligence-quality imagery resolution, and purposeful space object maneuvering techniques. The evaluation allows a maximum of 3.5 total points across the three factors, with weights assigned to each criterion. Offerors must submit their self-scoring by the response deadline of 1600 PST on 4 November 2025, with the ultimate goal of competing for a firm fixed-price contract to define, design, and build space-based technologies for the Space Domain Awareness mission area.
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Other files
| File | Type | Posted |
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| ATT 06_DRAFT Andromeda SF 328.pdf | ||
| ATT 19_DRAFT ROM Cost Template.xls | XLS spreadsheet | |
| ATT 24_DoDD 520502E.pdf | ||
| ATT 25_NIST SP 800-171 Rev 3.pdf | ||
| DRAFT Solicitation - FA881926RB001.pdf | ||
| Comment Resolution Matrix.xlsx | XLSX spreadsheet | |
| ATT 02_DRAFT HTRO Self-Score Matrix.xlsx | XLSX spreadsheet |
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Instructions
| General Instructions | |
| 1 | All Offerors shall fill in the yellow shaded cells for the General Score Sheet. Official scores for the purposes of determining an Offeror's score or the Government's assessment of that score in support of any award determination will be based on the General Score Sheet. |
| 2 | Offerors shall not modify or make any changes to other cells within the spreadsheet, including content, formulae, format. |
| 3 | Counts in this score matrix are binary. If a factor is met, then 1 would be the appropriate choice. If a factor is not met, then 0 would be the appropriate choice. |
| Scoring Category Instructions | |
| Factor 1: | |
| Demonstrated Prime/Lead Integrator for a GEO SV | EVALUATION BASIS: The offeror has served as the prime/lead integrator on a GEO space vehicle (SV) that has launched within the last 5 years or will be available for launch (AFL) within the next 24 months, in comparison to the release date of this RFP. |
Specific Guidance:
1) Prime/Lead Integrators are the primary party responsible for the effort, managing subsystem providers, and controlling the project from start to finish.
2) GEO has a specific altitude of approximately 35,786 kilometers (22,236 miles) above mean sea level.
3) The GEO SV must be ESPA class or larger.
4) If leveraging a GEO SV that will be AFL within the next 24 months, then the evidence must clearly demonstrate AFL within the next 24 months.
Factor 2:
Demonstrated Prime/Lead Integrator for a Space-Based Electro-Optical SV System EVALUATION BASIS: The offeror has served as the prime/lead integrator on at least one (1) space-based E/O system that produces space domain awareness (SDA) resolved image data that has, in comparison to the release date of this RFP, successfully launched within the last 5 years or will be available for launch (AFL) within the next 24 months.
Specific Guidance:
1) Prime/Lead Integrators are the primary party responsible for the effort, managing subsystem providers, and controlling the project from start to finish.
2) SDA resolved image data shall be taken to mean high resolution imagery, or imagery that provides intelligence quality resolution.
3) For systems that have not successfully launched within the last 5 years but will be available for launch (AFL) within the next 24 months, the offeror will clearly demonstrate with their work samples that the system will be AFL within the next 24 months.
| Factor 3: | |
| Demonstrated Prime/Lead Integrator for Rendezvous and Proximity Operations (RPO) SV System | EVALUATION BASIS: The offeror has served as the prime/lead integrator on at least one (1) space vehicle system that is capable of employing a rendezvous and proximity operations (RPO) suite that has, in comparison to the release date of this RFP, successfully launched within the last 5 years or will be available for launch (AFL) within the next 24 months. |
Specific Guidance:
1) Prime/Lead Integrators are the primary party responsible for the effort, managing subsystem providers, and controlling the project from start to finish.
2) Rendezvous and proximity operations are the purposeful maneuvering of one or more independent space object(s) to within close "proximity" of a RSO, via various rendezvous techniques to include sensors, orbital dynamics techniques, processing and data fusion, and hardware.
3) For systems that have not successfully launched within the last 5 years but will be available for launch (AFL) within the next 24 months, the offeror will clearly demonstrate with their work samples that the system will be AFL within the next 24 months.
DRAFT
Column Explanation
| Top Section | ||
| Column | Column Title | Explanation |
| B | Factor | Factor Number |
| C | Scoring Criterion | Summarized description of the scoring criterion. All the instructions are contained in this excel file. |
| D | INTENTIONALLY BLANK | |
| E | Maximum Count | The highest allowable count an Offeror can enter. |
| F | Offeror's Count | Offeror's count for each factor / criterion, in accordance with corresponding description and instructions in this file. OFFERORS FILL IN THIS INFORMATION |
| G | Weight Factor | Weight factor assigned to this factor / criterion |
| H | Max Possible Points | The maximum possible score an Offeror can receive in each factor / criterion. The sum of all values in this Column is the "Total Max Possible Points" in the "General Scoring Categories Total" that an Offeror can achieve for evaluation purposes. |
| I | Offeror's Self Score | Mathematically derived by multiplying Column F (Offeror's Count) by Column G (Weight Factor). This represents the Offeror's score for each category. The sum of all values in this Column is the Offeror's "General Scoring Categories Total" |
| J | USG Count | Reserved for Government Evaluator use. If the Government finds discrepancies during validation of Offeror provided counts, the Government reserves the right to reduce the score to align with validated information provided by the Offeror. See Section M for further details. |
| K | USG Evaluated Score | Mathematically derived by multiplying Column J (USG Count) by Column G (Weight Factor). This represents the Government's validated score for each category/criterion. The sum of all values in this Column is the Offeror's "Total USG Evaluated Score" in the "General Scoring Categories Total". |
&"Calibri,Regular"&10&K737373DRAFT
General Score Sheet
| Andromeda IDIQ | ||
| Solicitation Number: FA881926RB001 | Offeror Name: | |
| HTRO Self-Score Matrix |
| Factor | Scoring Criterion | Maximum Count | Offeror's Count | Weight Factor | Max Possible Points | Offeror's Self Score | USG Count | USG Evaluated Score |
| Factor 1 | The offeror has served as the prime/lead integrator on a GEO space vehicle (SV) that has launched within the last 5 years or will be available for launch (AFL) within the next 24 months, in comparison to the release date of this RFP. | 1.0 | 1.5 | 1.5 | 0.0 | 0.0 |
Factor 2 The offeror has served as the prime/lead integrator on at least one (1) space-based E/O system that produces space domain awareness (SDA) resolved image data that has, in comparison to the release date of this RFP, successfully launched within the last 5 years or will be available for launch (AFL) within the next 24 months. 1.0 1.0 1.0 0.0 0.0
Factor 3 The offeror has served as the prime/lead integrator on at least one (1) space vehicle system that is capable of employing a rendezvous and proximity operations (RPO) suite that has, in comparison to the release date of this RFP, successfully launched within the last 5 years or will be available for launch (AFL) within the next 24 months. 1.0 1.0 1.0 0.0 0.0
General Scoring Categories Total 3.5 0.0 0
DRAFT
File details come from the government source that posted it. Updated .