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Small Spacecraft Technology

Small Vehicle Experimental Launch Testbed (SVELT)

Completed Technology Project

Project Introduction

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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Project Duration

Technology Maturity (TRL)

Technology Areas

Target Destination

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