SBIR/STTR Research Award

Magnetohydrodynamic Energy Bypass Application for Single-Stage-to-Orbit Vehicles

Award identifier 2f357e9c39a8357474085fc231bb50e68d58e6df646b8b2198c3a61eb4ffa977Awarding agency National Aeronautics and Space Administration

Award amount

$0

Program and phase

SBIR · Phase I

Award year

2001

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Mse Technology Applications, Inc.
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research abstract

The global political structure has changed dramatically since the breakup of the former Soviet Union. World changes have caused the U.S. to reprioritize its National hypersonic needs. The United States government has looked to the needs of the future, and the hypersonic aeorospace plane is one of the systems included in alternative force structures. One of the hypersonic aerospace plane concepts would involve magnetohydrodynamic (MHD) technology, or the AJAX hypersonic flight vehicle concept, originally proposed by Russian scientist Vladimir Fraishtadt. The objective of this proposal is to study an air-breathing horizontal take-off and landing design concept using an MHD energy bypass injector ramjet engine. MSE and Hypertech Concepts will be using MSE developed Electromagnetic code (MSEID Code) with new Scramjet model and other tools to examine the total system performance. Both cruiser and space launch propulsion configurations will be investigated. The MSE and Hypertech Concepts team will make sure this propulsion and operational concept for the hypersonic aerospace plane is based on operations consistent with existing NASA goals. The overall operational concept will also be examined to determine the overall cost effectiveness.

Technology keywords

Not reported

Agency intelligence

National Aeronautics and Space Administration

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