OUSD (R&E) CRITICAL TECHNOLOGY AREA(S): Space Technology The technology within this topic is restricted under the International Traffic in Arms Regulation (ITAR), 22 CFR Parts 120-130, which controls the export and import of defense-related material and services, including export of sensitive technical data, or the Export Administration Regulation (EAR), 15 CFR Parts 730-774, which controls dual use items. Offerors must disclose any proposed use of foreign nationals (FNs), their country(ies) of origin, the type of visa or work permit possessed, and the statement of work (SOW) tasks intended for accomplishment by the FN(s) in accordance with section 3.5 of the Announcement. Offerors are advised foreign nationals proposed to perform on this topic may be restricted due to the technical data under US Export Control Laws. OBJECTIVE: This topic seeks to develop an expendable low-cost separation system for space payload deployment agnostic of Launch Service Provider (LSP) and cargo container providers. The goal is to create concepts that prioritize affordability and sufficient reliability and quality without resorting to complex or specialized designs. Proposed solutions may include mechanical, electrical, explosive, or other innovative non-traditional methods, emphasizing simplicity and cost-effectiveness. DESCRIPTION: This Phase I effort seeks to develop an expendable, low-cost separation system that is agnostic of Launch Service Providers (LSPs) and cargo container providers. The focus is on minimizing costs while ensuring sufficient reliability and quality without relying on complex or highly specialized designs. Proposed concepts may include mechanical, electrical, explosive, or other non-traditional methods. Emerging technological advancements provide a significant opportunity for the Department of the Air Force (DAF) to enhance Rocket Cargo materiel transport missions through improved post-atmospheric reentry payload deployment. The production of separation systems is inherently complex and costly, with development traditionally limited to a small number of suppliers restricting innovation and growth in the space industry. This initiative aims to shift away from costly, specialized designs toward innovative approaches in design, fabrication, and testing that support reliable payload survivability in the 1 to 10 metric ton range. The goal is to establish a versatile, expendable separation system compatible with any LSP and cargo container, broadening application across multiple space platforms and reducing the overall expense of payload deployment. Concepts should prioritize simplicity, affordability, and adequate reliability. PHASE I: The objective of Phase I is to demonstrate the feasibility of a low-cost Separation System concept or conduct a comprehensive feasibility study assessing Separation System effectiveness relative to cost. This effort should explore innovative approaches that enable low cost, expendable, launch vehicle agnostic Separation System to enable survivability of payloads during atmospheric reentry, particularly for payload masses in the 1 to 10 metric ton range. Offerors should: - Propose a clear technical approach for a Separation System or feasibility study of the Separation System performance with cost reduction. - Include preliminary modeling, simulation, or experimental plans to evaluate Separation System characteristics. - Identify key materials, fabrication methods, and production scalability considerations. - Provide an initial assessment of manufacturing pathways and potential barriers to Low-Rate Initial Production (LRIP). - Discuss potential risks and mitigation strategies related to Separation System performance, manufacturing, or cost. Deliverables may include: - A comprehensive feasibility study report detailing Separation System performance relative to cost. - Conceptual designs or prototype descriptions illustrating the Separation System approach. - Preliminary Separation System modeling or test data supporting performance claims. - A manufacturing and fabrication pathway including material choices, production methods, and cost estimates. - Identification of technical and production challenges, along with proposed solutions for Phase II development. This Phase I effort will establish a foundational understanding and pathway for advancing the proposed Separation System solution toward LRIP and eventual operational use. PHASE II: The Phase II effort will focus on advancing the research and development effort initiated in Phase I. The Phase II project aims at maturing the design and/or concept from the Phase I-like effort and possibly a prototype to conduct research and testing in lab and realistic environments to provide essential data to address any technical challenges, safety concerns, regulatory requirements, and/or other concerns. Awardee(s) should also identify any challenges for Full-Rate Production (FRP). The Phase II objective is to advance the development and maturation of the Separation System concept developed in Phase I. The goal is to create and demonstrate a prototype capable of meeting Separation System requirements for atmospheric reentry payloads in relevant operational environments, while addressing manufacturability, cost, and safety considerations. Key Goals: - Develop and refine Separation System designs or concepts based on Phase I findings. - Fabricate a prototype system suitable for testing in laboratory and realistic operational conditions. - Conduct rigorous testing to evaluate Separation System performance, structural integrity, durability, and compliance with safety and regulatory standards. - Address technical challenges identified in Phase I, including material selection, fabrication methods, and integration strategies. - Assess manufacturability and scalability to enable transition toward Low-Rate Initial Production (LRIP) and Full-Rate Production (FRP). - Identify and mitigate potential barriers to production, safety, and operational deployment. Deliverables May Include: - Detailed prototype design documentation and fabrication plans. - Test plans and protocols for laboratory and operational environment evaluation. - Comprehensive test reports documenting Separation System performance, safety, durability, and regulatory compliance. - Updated risk assessment and mitigation strategies based on test results. - Manufacturing and production feasibility studies, including cost analysis. - Recommendations and pathways for LRIP and FRP phases, including any identified production or safety challenges. PHASE III DUAL USE APPLICATIONS: The Phase III effort aims to demonstrate the separation system in an operational-like environment and achieve technology maturation and commercialization. The objective of Phase III is to demonstrate the expendable, low-cost separation system in an operational-like environment to achieve full technology maturation and enable commercialization. The effort will focus on validating system performance, reliability, and integration capabilities for both military and commercial space applications. Military applications: - Provide the Department of the Air Force (DAF) and other DoD agencies with a reliable, cost-effective separation system compatible with multiple Launch Service Providers (LSPs) and cargo containers. - Support Rocket Cargo materiel transport delivery missions, rapid deployment scenarios, and other space operations requiring expendable separation solutions. - Enhance operational agility and reduce lifecycle costs associated with payload deployment and separation. - Enable scalable production to meet increasing mission demands. Commercial Applications: - Facilitate flexible payload integration across a variety of commercial cargo containers and launch platforms. - Reduce costs for commercial space operators by providing an expendable, simplified separation mechanism that maintains sufficient reliability and quality. The end goal is to establish a versatile, low-cost, and expendable separation system that broadens the industrial base, reduces mission costs, and supports a wide range of military and commercial space materiel transport operations, fostering innovation and ensuring sustainable space mission success. REFERENCES: 1. SpaceX Falcon 9 Payload Users Guide (PUG) - https://www.spacex.com/media/falcon-users-guide-2021-09.pdf. 2. Rocket Lab Neutron Payload Users Guide (PUG) - https://rocketlabcorp.com/assets/Uploads/Rocket-Lab-Neutron-PUG-reduced-final.pdf. 3. Motorized Lightband - https://www.rocketlabusa.com/space-systems/separation-systems/motorized-lightband/. 4. Planetary Systems Corporation Motorized Lightband - https://satsearch.co/products/planetarysystemscorp-mark-ii-motorized-lightband. KEYWORDS: Space separation system, low cost, expendable, space payload deployment, modular separation system, atmospheric reentry, Rocket Cargo materiel transport, launch vehicle agnostic, payload survivability, space mission affordability
