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reportActive / Technical Report | Accession Number: ADB816663 | Open PDF

Abstract:

The document is the first progress report on an investigation of guidance, propulsion, launching, and supersonic aerodynamics leading to the design of a ground-to-air guided missile, capable of intercepting and destroying hostile aircraft operating at altitudes up to 500,000 feet, at speeds up to 4,000 mph, and at ranges sufficient to prevent damage to the defended area. The report deals with the kinds of problems being considered in the various phases of the work.

Author(s):
No Author(s) Identified
Author Organization(s):
MICHIGAN UNIV ANN ARBOR ENGINEERING RESEARCH INST
Descriptive Note:
Progress rept. no. 1, 3 Apr-1 Jun 1946
Supplementary Note:
Ground-to-air pilotless aircraft research program.
Pagination:
0026

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

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

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
UMR-1
Contract/Grant Number(s):
W33-038-AC-14222
Project Number(s):
MX-794
Monitor Series:
AMC-AF
 Subject Terms
Joint Capability Areas:
JCA_3_Force Application; JCA_3.1.1_Maneuver to Engage; JCA_3.1_Maneuver; JCA_3.2_Engagement; JCA_3.2.1_Kinetic Means; JCA_5_Command and Control; JCA_1.2_Force Preparation; JCA_1_Force Support; JCA_6_Net Centric; JCA_1.2.3_Educating; JCA_5.3_Planning
Communities of Interest:
Weapons Technologies
Descriptor(s):
*GUIDED MISSILES, AERODYNAMIC CHARACTERISTICS, ANTIAIRCRAFT MISSILES, LAUNCHING, PROPULSION SYSTEMS, SUPERSONIC CHARACTERISTICS, SURFACE TO AIR MISSILES
Field(s)/Group(s):
Guided Missiles
Keyword(s):
ATI 671, ATI COLLECTION
Report Date:
1946 Jun 01
Creation Date:
2010 Mar 03