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Small Spacecraft Technology

Small Vehicle Experimental Launch Testbed (SVELT)

Completed Technology Project
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Project Description

Small Vehicle Experimental Launch Testbed

The overall technical objective of the present study is to perform an engineering assessment of an F-4 aircraft with WIPCC to launch at supersonic speed a rocket-powered launch vehicle carrying a small payload

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Anticipated Benefits

Primary U.S. Work Locations and Key Partners

Technology Transitions

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