Media Information

 
 
 
Collection:
NASA Great Images in Nasa Collection
Title:
Cold-Flow Propulsion Research Test
Full Description:
An engineer at the Marshall Space Flight Center (MSFC) Wind Tunnel Facility uses lasers to measure the velocity and gradient distortion across an eight inch curved pipe with joints and turning valves during a cold-flow propulsion research test; simulating the conditions found in the X-33's hydrogen feedline. Lasers are used because they are non-intrusive and do not disturb the flow like a probe would. The feedline supplies propellants to the turbo pump. The purpose of this project was to design the feedline to provide uniform flow into the turbo pump.
Date:
12/11/1997
NASA Center:
Marshall Space Flight Center
Subject Category:
Rocket Propulsion
Keywords:
Propulsion
Keywords:
X-33
Keywords:
Laser
Audience:
General Public
facet_where:
Marshall Space Flight Center (MSFC)
facet_when:
12-11-1997
facet_when_year:
1997
Image #:
9712449
original_url:
UID:
SPD-GRIN-GPN-2000-00 0068
Center:
MSFC
Center Number:
9712449
GRIN DataBase Number:
GPN-2000-000068
Creator-Photographer:
NASA Terry Leibold
Original Source:
DIGITAL

Cold-Flow Propulsion Research Test