Atlas/Agena Flight Test Directive for Atlas 110D,

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Abstract:

The purpose of the GDA FTD is to provide a working document to define objectives and to set forth evaluation criteria, preparations and support requirements for the pre-launch and launch portion of the Atlas Booster for each Atlas Agena flight test. Author

Author(s):
Cole, D. E.
Author Organization(s):
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Pagination:
0100

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
GDA-A62-521-73, GDA-ESG-814
 Subject Terms
Joint Capability Areas:
JCA_5.3_Planning; JCA_5_Command and Control
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*LAUNCH VEHICLES, OPERATIONAL READINESS, LAUNCHING SITES, PROPELLANT TRANSFER, AUTOMATIC PILOTS, INERTIAL GUIDANCE, PNEUMATIC EQUIPMENT, HYDRAULIC EQUIPMENT, GUIDED MISSILE TRACKING SYSTEMS, GUIDED MISSILE SAFETY
Field(s)/Group(s):
Ground Support Systems and Facilities for Space Vehicles
Keyword(s):
AGENA, ATLAS LAUNCH VEHICLES, MISSILE MODIFICATION
Report Date:
1962 Mar 27