SBIR/STTR Research Award

A 128-Channel Compact VUV Spectrometer for Wide-Temperature Entry Descent & Landing Sensing Applications

Award identifier 510d0871d1fe6b94bd809f6c42b4839126a50a225b66b261f246540dd5066847Awarding agency National Aeronautics and Space Administration

Award amount

$124,998

Program and phase

SBIR · Phase I

Award year

2018

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
OZARK INTEGRATED CIRCUITS INC
Proposal award date
2018-07-27
Contract end date
2019-02-15
UEI
C3JNF19C7DK8
Solicitation number
SBIR_18_P1
Topic code
Z7

Research abstract

NASA manned and robotic missions to the surface of planetary or airless bodies require Entry, Descent, and Landing (EDL). For many of these missions, EDL represents one of the riskiest phases of the mission. Despite the criticality of the EDL phase, NASA has historically gathered limited engineering data from such missions, and use of the data for real-time Guidance, Navigation and Control (GN&C) during EDL for precise landing (aside from Earth) has also been limited.NASA scientists have identified a compact vacuum ultraviolet spectrometer as a key enhancement to EDL sensing.Ozark IC has developed a far-ultraviolet focal plane array (FPA) in SiC BiCMOS technology. The 159x64 pixel FPA has a spectral response from 100[JH1] nm to 350 nm. BiCMOS test circuits in this technology have demonstrated operation for 100 hours at 500ºC suggesting this FPA will not require any active cooling to operate. The key feasibility question to be answered is: Can the high-temperature packaging and optics be designed with a maximum dimension of 10 centimeters?The primary objective is to answer the feasibility question through a series of measurement and design tasks. Ozark IC will developsupporting FPA firmware and software for environmental testing of the FPA. LumenFlow will then design the spectrometer optics for the smallest possible form factor. Ozark IC will apply it’s high-temperature ceramic packing solutions to design a high-temperature substrate and connector system for the SiC FPA and investigate enclosure materials.Objectives of Phase IDetermine coldest possible operating temperature of the SiC FPA (cryogenic testing)Operate the SiC FPA as a spectrometer using representative spectral linesInvestigate design trade-offs of thermally matched ceramic substrates for SiC FPA ASICDesign compact spectrometer components and verify with optical simulationDesign VUV experiments to validate the optical system and identify design apparatus needed to complete the experiment

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

37 SBIR/STTR records share this UEI (2012–2024). Reported award amounts total $19,866,110. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Energy, National Aeronautics and Space Administration, Department of Defense, National Science Foundation

Agency intelligence

National Aeronautics and Space Administration

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