SBIR/STTR Research Award

Composite Cryogenic Hydrogen Insulated Lightweight Lined Storage (C-CHILL)

Award identifier 2fb08e85c625c96a20e28fd1ae15f6627abc4e031740d9a0440fd88cc12c6788Awarding agency National Aeronautics and Space Administration

Award amount

$149,998

Program and phase

SBIR · Phase I

Award year

2023

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
DYNOVAS INC
Proposal award date
2023-08-01
Contract end date
2024-02-02
UEI
WJX9FRCLNFQ5
Solicitation number
SBIR_23_P1
Topic code
Z10

Research abstract

Dynovasrsquo; Composite Cryogenic Hydrogen Insulated Lightweight Lined (C-CHILL) storage system provides a novel solution that specifically addresses NASArsquo;s call for development of liquid hydrogen compatible composite tanks for reusable systems such as spacecraft, surface systems, and hydrogen aircraft for long-duration storage of liquid hydrogen. The solution was developed based on previous technologies that have been proven for cryogenic storage, and advances on the state of the art to achieve long-duration cryogenic fluid storage.nbsp;Dynovasrsquo; C-CHILL is scalable for a wide range of applications spanning aircraft, spacecraft, landers, rovers, launch vehicles, and refueling tanks.Dynovasrsquo; proposed C-CHILL tank design leverages proven cryogenic hydrogen storage technologies and processes,nbsp;and incorporates additional improvements to achieve a mass-efficient structural design fornbsp;long duration storage with improved lifecycle capability. These include:Thin Ply Composite Materials ndash; Toughened thin-ply composite materials that allow an increased number of cross laminates in the composite overwrap, greatly reducing microcrackingVacuum Jacketed Insulation ndash; Vacuum insulated layer including composite honeycomb core and MLI between the inner and outer tanks, acting as a structural member and thermal barrierTrapped Polymer Liner ndash; Polymer liner designed for use at cryogenic temperatures, retained within the composite laminate greatly reducing hydrogen permeation through the tank wallsNanomaterial Integration ndash; Integration of thin-walled carbon nanotubes within the matrix during winding to increase micro-crack resistance, by increasing strength and toughnessUsing these technologies together, Dynovasrsquo; C-CHILL will advance cryogenic hydrogen storage solutions to achieve long-duration storage with improved life-cycle capability, accounting for use cases requiring gt;5,000 pressure cycles at cryogenic temperatures (20K), and gt;10,000 thermal cycles between 20K and 300K.nbsp;

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

44 SBIR/STTR records share this UEI (2020–2025). Reported award amounts total $25,640,997. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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