Thermal & Mechanical Design for Spaceflight Camera

The contract involves the design of mechanical and thermal interfaces specifically aimed at maintaining the temperature of a spaceflight camera body within the range of +20°C to +30°C during operation. The design must utilize black anodized aluminum to meet thermal requirements and ensure compatibility with radiation exposure conditions, specifically withstanding radiation levels below 18 krad when shielded with 100 mils of aluminum. This work is a subcontract opportunity posted by NASA Shared Services Center, with a response deadline set for June 17, 2026. The scope requires expertise in thermal management and materials compatible with space environments, focusing on the delicate balance between effective heat control and radiation survivability for spaceflight applications. The contract is classified under NAICS code 332996, which relates to metal heat treating, emphasizing the technical nature of the mechanical and thermal design to be delivered. Although the specific location for performance is not provided, the solicitation clearly targets suppliers capable of supporting NASA’s mission-critical components for space operations.