NASA Langley Research Center - Multimedia Repository
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New Multimedia
Title:
British Swallow - Variable Sweep Model
ID #:
EL-2008-00002
Format:
IMAGE (JPEG 544x334)
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Title:
Dr. John Stack and other NASA Langley Research Center Visitors
ID #:
EL-2008-00001
Format:
IMAGE (JPEG 544x435)
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Title:
Planet Mars from Viking Orbiter 1
ID #:
EL-2001-00436
Format:
IMAGE (JPEG 544x464)
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Title:
Experimental Ablation Cooling
ID #:
LV-2007-00001
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Aerodynamic Heating of Blunt Nose Shapes at Mach Numbers up to 14
ID #:
LV-2007-00002
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Reentry Body Stability Tests Conducted in Langley Spin Tunnel
ID #:
LV-2007-00003
Format:
MOVIE (QUICKTIME 196x144)
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Title:
8-Inch Diameter Rigid Parachute Model of the Cook Research Laboratory
ID #:
LV-2007-00004
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Water Landing Characteristics of a Reentry Capsule
ID #:
LV-2007-00005
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Studies of Accelerations in Manned Vehicles During Exit and Reentry Flight
ID #:
LV-2007-00006
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Flow Studies of Decelerators at Supersonic Speeds
ID #:
LV-2007-00007
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Dynamic Model Tests of Models in the McDonnell Design of Project Mercury Capsule
ID #:
LV-2007-00008
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Dynamic Model Tests of Models of the McDonnell Design of Project Mercury Capsule
ID #:
LV-2007-00009
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Water Landing Characteristics of a 1/6-Scale Model Reentry Capsule with an 80-Inch Heat Shield
ID #:
LV-2007-00010
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Thermo-Lag Ablation Tests
ID #:
LV-2007-00011
Format:
MOVIE (QUICKTIME 196x144)
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td>
Title:
Landing Energy Dissipation for Manned Reentry Vehicles
ID #:
LV-2007-00012
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Flow About Reefed Parachute Models Towed at Supersonic Speeds Behind a Conical Body
ID #:
LV-2007-00013
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Tests of Vortex-Ring Parachute at Supersonic Speed in the Langley Unitary Plan Wind Tunnel
ID #:
LV-2007-00014
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Flow Over Blunt Body at M equals 20 in 2-Inch Helium Tunnel
ID #:
LV-2007-00015
Format:
MOVIE (QUICKTIME 196x144)
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Title:
High-Speed Schlieren Movies of Decelerators at Supersonic Speeds
ID #:
LV-2007-00016
Format:
MOVIE (QUICKTIME 196x144)
Details:
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Title:
High Speed Schlieren Studies of Flow Over Mercury Atlas Vehicle
ID #:
LV-2007-00017
Format:
MOVIE (QUICKTIME 196x144)
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Title:
1/9-Scale Saturn Model
ID #:
LV-2007-00018
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Aerodynamic Characteristics of Parachutes at Mach Numbers from 1.6 to 3
ID #:
LV-2007-00019
Format:
MOVIE (QUICKTIME 196x144)
Details:
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Title:
Landing of Manned Reentry Vehicles
ID #:
LV-2007-00020
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Effect of Load-Alleviating Structure on the Landing Behavior of a Reentry-Capsule Model
ID #:
LV-2007-00021
Format:
MOVIE (QUICKTIME 196x144)
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Title:
Wind Tunnel Investigation of a Balloon as Decelerator at Mach Numbers from 1.47 to 2.50
ID #:
LV-2007-00022
Format:
MOVIE (QUICKTIME 196x144)
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NASA Official:
Bill von Ofenheim (LARC-DL-lisar@mail.nasa.gov)
Date:
04/07/2008