Initial Acceptance Test Report for Regulator Assembly, 'E' Series Helium Pressure (Liquid Oxygen Tank) Dwg. No. 27-80400 (Convair Stratos),

reportActive / Technical Report | Accession Number: AD0843522 | Need Help?

Abstract:

The purpose of this report is to describe the test equipment and procedure required for the initial acceptance testing of a liquid oxygen tank pressure regulator in a simulated missile propellant tank flow set-up. Author

Author(s):
Ryan, H. P.
Author Organization(s):
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Pagination:
0309

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release, Document Partially Illegible
Distribution Statement:
Document Partially Illegible.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
GDA-27A685-1
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application
Communities of Interest:
Weapons Technologies
Descriptor(s):
*SURFACE TO SURFACE MISSILES, *PRESSURE REGULATORS, MATHEMATICAL MODELS, VIBRATION, CONTROL SYSTEMS, PERFORMANCE(ENGINEERING), PROPELLANT CONTROL, LIQUID ROCKET OXIDIZERS, PROPELLANT TANKS, LEAKAGE(FLUID), RESONANT FREQUENCY, PRESSURIZATION
Field(s)/Group(s):
Test Facilities, Equipment and Methods, Surface-Launched Guided Missiles, Liquid Propellant Rocket Engines
Keyword(s):
atlas, ullage, xsm 65e missiles
Report Date:
1961 Feb 13
Creation Date:
1969 Jan 15