Evaluation Test of A/B Regulator Performance During Simulated APCHE Checkout.

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Abstract:

The object of this test was to determine the fluid medium, the flow rate, and the upstream pressure required by the airborne tank pressure regulators to assure non-cyclic regulator performance when flowing into a fixed ullage of 43 cubic feet for the LO2 tank regulators and 27 cubic feet for the fuel tank regulators. Author

Author(s):
Melvin, D. J.
Author Organization(s):
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Pagination:
0028

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
GDA-27A1244
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*PROPELLANT TANKS), (*SURFACE TO SURFACE MISSILES, (*PNEUMATIC SERVOMECHANISMS, PERFORMANCE(ENGINEERING)), PROPELLANT TRANSFER, PRESSURE REGULATORS, CHECKOUT PROCEDURES, SIMULATION, DETECTORS, PRESSURIZATION, BLEED SYSTEMS, ORIFICES, LEAKAGE(FLUID), TRANSDUCERS, RELIABILITY(ELECTRONICS)
Field(s)/Group(s):
Hydraulic and Pneumatic Equipment, Surface-Launched Guided Missiles, Liquid Rocket Propellants
Keyword(s):
AUTOMATIC PROGRAMMED CHECKOUT, ULLAGE
Report Date:
1961 Nov 16