PROPULSION RESEARCH LABORATORY SUMMARY REPORT FOR FY 1964.

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Abstract:

The APL Propulsion Research Laboratory constitutes a versatile blowdown facility for the implementation of exploratory development of advanced propulsion systems. Because of its ability to simulate the environmental conditions of high-speed flight, the facility has also been extended to implement experiments on ablation, heat transfer, and wake studies associated with missile re-entry. This is the first of what is intended to be a series of annual progress reports it covers the period of October 1, 1963 until September 30, 1964. Author

Author(s):
Olsen, H. L. ; Baker, W. T. ; Bunt, E. A.
Author Organization(s):
JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB
Descriptive Note:
Annual progress rept. no. 1, 1 Oct 63-30 Sep 64,
Annotation:
Propulsion research laboratory summary report for FY 1964.
Pagination:
0065

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
TG-734
Contract/Grant Number(s):
NOw-62-0604
Project Number(s):
Y1F
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application
Communities of Interest:
Weapons Technologies
Descriptor(s):
(*NAVAL RESEARCH, *RESEARCH MANAGEMENT), LABORATORIES, ARC HEATERS, THRUST AUGMENTATION, COMBUSTION, HYPERSONIC WIND TUNNELS, SUPERSONIC FLOW, SCHEDULING, BUDGETS, ABLATION, HEAT TRANSFER, TEST FACILITIES, ATMOSPHERE ENTRY, ENVIRONMENTAL TESTS, SAFETY, TEST EQUIPMENT, INSTRUMENTATION
Field(s)/Group(s):
Administration and Management, Test Facilities, Equipment and Methods, Fluid Mechanics
Keyword(s):
POLARIS, SCRAM
Report Date:
1965 Sep 01