Sensor Subsystem Assembly (SSA)
ID: RFI_GSFC_Sensor_Subsystem_Assembly_FY25GJEType: Sources Sought
Overview

Buyer

NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNASA GODDARD SPACE FLIGHT CENTERGREENBELT, MD, 20771, USA

NAICS

Search, Detection, Navigation, Guidance, Aeronautical, and Nautical System and Instrument Manufacturing (334511)

Original Source

https://sam.gov/opp/48d6aaf898844e8f97b27c5c2ce76595/view
Timeline
    Description

    NASA's Goddard Space Flight Center (GSFC) is seeking responses from industry vendors for a Short-wave Infrared (SWIR) Sensor Subsystem Assembly (SSA) intended for deployment in Low Earth Orbit as part of an Earth observing instrument. The SSA must meet specific technical requirements, including a target mass of approximately 1.5 kg, operational thermal ranges, and high-performance detection capabilities with defined pixel dimensions and a minimum frame rate. This initiative is crucial for advancing space exploration technologies and ensuring effective data collection in space environments. Interested vendors are invited to submit their responses, including pricing and technical documentation, via email to Steve Tompkins by January 31, 2024, referencing Sensor Subsystem Assembly ID # RFI_GSFC_Sensor_Subsystem_Assembly_FY25GJE.

    Point(s) of Contact
    Steve Tompkins
    steve.tompkins@nasa.gov
    Amy Aqueche
    amy.a.aqueche@nasa.gov
    Files
    Title
    Posted
    RFI_GSFC_Sensor_Subsystem_Assembly_FY25GJE.pdf
    NASA's Goddard Space Flight Center (GSFC) issued a Request for Information (RFI) seeking responses from industry vendors capable of providing a Short-wave Infrared (SWIR) Sensor Subsystem Assembly (SSA) for an Earth observing instrument. This RFI is for informational and planning purposes only and does not constitute a solicitation for proposals. The SSA is intended for deployment in Low Earth Orbit and must meet specific technical requirements, including mechanical, thermal, electrical, and performance criteria. Key details include a target mass of approximately 1.5 kg, operational thermal ranges, voltage requirements, and data handling specifications. The SSA must offer high-performance detection capabilities with specified pixel dimensions and a minimum frame rate, as well as withstand space radiation. Responses should include documentation highlighting relevant experience, proposed costs and schedules, and any prior flight heritage. Submissions are to be sent via email by January 31st, 2024, with specified referencing to ensure clarity. NASA emphasizes the importance of market input to verify feasibility and promote competition while ensuring no financial obligation for responses. This initiative reflects NASA's commitment to innovative collaboration with industry partners in advancing space exploration technologies.
    Lifecycle
    Title
    Type
    Sensor Subsystem Assembly (SSA)
    Currently viewing
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