Image:Twin Linear Aerospike XRS-2200 Engine edit scaled.jpg

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[edit] Summary

Testing of Twin Linear Aerospike XRS-2200 Engine (noise removed, downsampled)

Description

The test of twin Linear Aerospike XRS-2200 engines, originally built for the X-33 program, was performed on August 6, 2001 at NASA's Stennis Space Center, Mississippi. The engines were fired for the planned 90 seconds and reached a planned maximum power of 85 percent. NASA's Second Generation Reusable Launch Vehicle Program , also known as the Space Launch Initiative (SLI), is making advances in propulsion technology with this third and final successful engine hot fire, designed to test electro-mechanical actuators. Information learned from this hot fire test series about new electro-mechanical actuator technology, which controls the flow of propellants in rocket engines, could provide key advancements for the propulsion systems for future spacecraft. The Second Generation Reusable Launch Vehicle Program, led by NASA's Marshall Space Flight Center in Huntsville, Alabama, is a technology development program designed to increase safety and reliability while reducing costs for space travel. The X-33 program was cancelled in March 2001.
Source

http://nix.ksc.nasa.gov/info;jsessionid=8a9ofkryn0iy?id=MSFC-0103149&orgid=11
Date

August 6, 2001
Author

NASA Marshall Space Flight Center (NASA-MSFC) [1], edited by ed g2s • talk, downsampled by KFP.
Permission

PD-USGov-NASA
Other versions Image:Twin_Linear_Aerospike_XRS-2200_Engine.jpg (original), Image:Twin_Linear_Aerospike_XRS-2200_Engine_edit.jpg (edited)

[edit] Licensing

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