Critical Engine Components Minimum Temperature Study Missile 36D,

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Abstract:

The report presents the results of a critical engine components minimum temperature study using Missile 36D.

Author(s):
Ramsay, D. L.
Author Organization(s):
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Pagination:
0044

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
GDA-EM-1539
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means
Communities of Interest:
Weapons Technologies
Descriptor(s):
(*SURFACE TO SURFACE MISSILES, LIQUID PROPELLANT ROCKET ENGINES), (*ENGINE COMPONENTS, THERMAL ANALYSIS), HEAT TRANSFER, CAPTIVE TESTS, PROPELLANT TRANSFER, LUBRICANTS, ELECTRIC SWITCHES, CONTROL SYSTEMS
Field(s)/Group(s):
Thermodynamics, Liquid Propellant Rocket Engines
Keyword(s):
ATLAS, XSM 65D MISSILES
Report Date:
1960 May 20