SBIR/STTR Research Award

High Temperature Inflation Hoses and Ports for Next Generation Inflatable Heat Shields

Award identifier 31d2571fc670811d460739eedf516218f14fef65d1f2b56730277d3381264d76Awarding agency National Aeronautics and Space Administration

Award amount

$156,280

Program and phase

SBIR · Phase I

Award year

2024

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Jackson Bond Enterprises LLC
Proposal award date
2024-08-01
Contract end date
2025-02-06
UEI
THNCRQCNX8V8
Solicitation number
SBIR-2024-Phase 1
Topic code
Z7

Research abstract

NASA Langley Research Center (LaRC) led the successful flight test of a 6-meter diameter HIAD in November 2022 under the project called the Low earth Orbit Flight Test of an Inflatable Decelerator (LOFTID) project. This demonstration has led to new opportunities with commercial partners that require further scale-up of the deployable aeroshell technology. For example, NASA LaRC is developing a 10-meter diameter HIAD that is being considered for use by United Launch Alliance (ULA). Scaling the inflatable heat shield from LOFTID’s 6-meter to a 10-meter class and beyond will require solving manufacturing, design, and procurement challenges for several materials, components, and systems. The Inflatable Structure (IS) system of NASA’s 10m HIAD will benefit from larger hoses and ports than are currently available to inflate the heat shield. The hoses are located on the back side of the inflatable heat shield, somewhat protected from the front side heat pulse, yet must survive radiation from plasma trails and heat conduction through the heat shield during the ~5 min heat pulse. The hoses are expected to near peak external temperatures of 400C during reentry while the inside will need to resist hot gases from a gas-generator inflation system with gas temperatures up to 200C. JBE is proposing to demonstrate the design and manufacturing of a 1 inch and 2 inch diameter class hoses and ports, that can survive the requirements of an inflatable heat shield aeroshell component including packing and deployment, inflation load, max aerodynamic load, and the forementioned temperatures. The SOTA LOFTID hoses limit the inflation time of the inflatable heat shield. In PHI, JBE will focus on demonstrating the use of novel materials and manufacturing techniques to develop a 1 inch diameter class hose and port. In PHII, JBE will build upon the lessons learned in PHI, develop a 2 inch diameter class hose and port and validate the performance of both classes with thermo-mechanical testing.

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

8 SBIR/STTR records share this UEI (2019–2025). Reported award amounts total $4,192,450. Reported amounts are not federal obligations.

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

Agencies: National Aeronautics and Space Administration, Department of Defense

Agency intelligence

National Aeronautics and Space Administration

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