SBIR/STTR Research Award

Acoustic Igniter

Award identifier 626293c845931961b7d176b4219c16446ed423c049cbeb7be72a13fcf94d6f26Awarding agency National Aeronautics and Space Administration

Award amount

$599,994

Program and phase

SBIR · Phase II

Award year

2009

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Orion Propulsion, Inc.
Proposal award date
2009-09-30
Contract end date
2011-03-31
UEI
Not reported
Solicitation number
Not reported
Topic code
X9.03

Research abstract

An acoustic igniter eliminates the need to use electrical energy to drive spark systems to initiate combustion in liquid-propellant rockets. It does not involve the use of catalysts (which have a limited life), it does not exhibit typical wear and tear as seen in spark and catalytic igniters, and it is simple in design with no moving parts. Orion's proposed Acoustic Igniter is expected to offer a long-life, highly reliable ignition system that does not require high-voltage electrical connections. It is less complex to operate and simpler than a traditional ignition system. Orion's primary technical objective is to produce an acoustic igniter design that will ignite combustion of common liquid rocket fuel and oxidizer combinations such as gaseous oxygen and kerosene, and oxygen/methane. During Phase 1, we analyzed the operational issues that inhibit acoustic igniter performance. Based on these results, Orion will built a prototype unit, tested it, and evaluated its performance. This work established a basis for the follow-on Phase 2 effort to refine the design and upgrade the technology level of the acoustic igniter.

Technology keywords

Not reported

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Agency intelligence

National Aeronautics and Space Administration

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