NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
NASA Langley Unitary Plan Wind Tunnel - Entry, Descent, and Landing Project - Supersonic Retropropulsion Test - Test 1853 in Test Section 2, Conducted July 2010 - Mach 2.4, 3.5, 4.6 Schlieren VideosCompilations of high-speed schlieren videos showing supersonic retropropulsion in the Langley Unitary Plan Wind Tunnel at Mach 2.4, 3.5, and 4.6.
Document ID
20130008165
Acquisition Source
Langley Research Center
Document Type
Presentation
External Source(s)
http://youtu.be/fTmPc1olhiU
http://youtu.be/i-coJg_vgxI
http://youtu.be/-ezb03W6KCc
Authors
Berry, Scott A. (NASA Langley Research Center Hampton, VA, United States)
Wheless, Richard A. (NCI Information Systems, Inc. Hampton, VA, United States)
Date Acquired
August 27, 2013
Publication Date
October 16, 2012
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-15419
Report Number: NF1676L-15419
Funding Number(s)
WBS: WBS 432938.11.01.07.43.40.05
Distribution Limits
Public
Copyright
Public Use Permitted.

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available