Similar
A close up of a pair of cuff watches. Locks security padlocks.
COMPONENTS OF 2 STAGE LOKI 3-1 MISSILE
STS106-321-018 - STS-106 - Ventilation ducts and CBM interfaces in Node 1 and PMA2 during STS-106
HUBBLE MODEL PHOTO FOR COVER DESIGN
JT-8D UPSTREAM VIEW, NASA Technology Images
A large metal pipe in a building with a clock on the wall. Industry hall ventilation, work.
STS106-343-011 - STS-106 - External views of Node 1 taken from Atlantis during STS-106
Related
The Unitary Plan Wind Tunnel(UPWT) Test 1891 Space Launch System
The Unitary Plan Wind Tunnel(UPWT) Test 1891 Space Launch System
The Unitary Plan Wind Tunnel(UPWT) Test 1891 Space Launch System
The Unitary Plan Wind Tunnel(UPWT) Test 1891 Space Launch System
The Unitary Plan Wind Tunnel(UPWT) Test 1891 Space Launch System
The Unitary Plan Wind Tunnel(UPWT) Test 1891 Space Launch System
The Unitary Plan Wind Tunnel(UPWT) Test 1891 Space Launch System
The Unitary Plan Wind Tunnel(UPWT) Test 1891 Space Launch System
The Unitary Plan Wind Tunnel(UPWT) Test 1891 Space Launch System
The Unitary Plan Wind Tunnel(UPWT) Test 1891 Space Launch System
Summary
Stage Separation Test of the Space Launch System(SLS) in the Langley Unitary Plan Wind Tunnel (UPWT). The model used High Pressure air blown through the solid rocket boosters. (SRB) to simulate the booster separation motors (BSM) firing.
Tags
sls
space launch system
solid rocket booster
lrc
george homich lamps contract
langley research center
unitary
plan
wind
tunnel
unitary plan wind tunnel
upwt
test
space
launch
system
high resolution
rocket engines
rocket technology
nasa
experimental aircraft
Date
2000 - 2020
Location
Langley Research Center
,
37.09672, -76.38312
Source
NASA
Link
Copyright info
Public Domain Dedication (CC0)