NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
External Tank GH2 Vent ArmBecause the venting of free hydrogen gas to the atmosphere presents an extremely hazardous situation, it was necessary to devise a means for safe, controlled venting of the shuttle external tank gaseous hydrogen during and after liquid hydrogen tank loading. Several design concepts that were considered initially were discarded as unfeasible because of vehicle weight restrictions, high cost, and because the proposed structure was itself deemed a hazard due to the vehicle's nonvertical launch trajectory. These design concepts are discussed. A design employing a support structure/access arm attached to the fixed service structure was finally selected. The various design problems resolved included vent arm disconnect/drop interference, minimizing refurbishment due to launch damage, disconnect reliability, vehicle movement tracking, minimizing vent line pressure drop, and the presence of other vehicle services at the same centralized supply area. Six launches have proven the system to be reliable, efficient, and of nearly zero refurbishment cost.
Document ID
19850008660
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reichle, G. E.
(NASA John F. Kennedy Space Center Cocoa Beach, FL, United States)
Glassburn, C. W.
(Planning Research Corp. Kennedy Space Center, Fla., United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA. Johnson Space Center Space Shuttle Tech. Conf., Pt. 2
Subject Category
Space Transportation
Accession Number
85N16969
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available