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Purging of a tank-mounted multilayer insulation system by gas diffusionThe investigation was conducted on a multilayer insulation (MLI) system mounted on a spherical liquid hydrogen propellant tank. The MLI consisted of two blankets of insulation each containing 15 double-aluminized Mylar radiation shields separated by double silk net spacers. The gaseous nitrogen initially contained within the MLI system and vacuum chamber was purged with gaseous helium introduced both underneath the MLI and into the vacuum chamber. The MLI panels were assumed to be purged primarily by means of gas diffusion. Overall, test results indicated that nitrogen concentrations well below 1 percent could be achieved everywhere within the MLI system. Typical times to achieve 1 percent nitrogen concentration within the MLI panels ranged from 69 minutes at the top of the tank to 158 minutes at the bottom of the tank. Four space-hold thermal performance tests indicated no significant thermal degradation of the MLI system had occurred due to the purge tests conducted. The final measured heat input attributed to the MLI was 7.23 watts as compared to 7.18 watts for the initial baseline thermal performance test.
Document ID
19780009184
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Sumner, I. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-TP-1127
E-9286
Report Number: NASA-TP-1127
Report Number: E-9286
Accession Number
78N17127
Funding Number(s)
PROJECT: RTOP 506-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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