AMR Weight History of the Atlas/Ranger (RA-1) Vehicle SM-65D-111.

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Abstract:

The purposes of the report are to present all data concerned with the determination of the final Atlas dry weight, Atlas propellant weight, and total gross weight of the Atlas Booster, SM-65D-111Agena B and Spacecraft RA-1 at significant times from Atlas ignition to Atlas vernier cutoff. Author

Author(s):
Sheeley, V. V.
Author Organization(s):
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Pagination:
0052

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release, Document Partially Illegible
Distribution Statement:
Availability: Microfiche Copies Only.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
GDA-AA61-0135
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*LAUNCH VEHICLES, WEIGHT, PAYLOAD, LIQUID ROCKET PROPELLANTS, BOOSTER ROCKET ENGINES, PROPELLANT TRANSFER, LUNAR PROBES, PROPELLANT CONTROL, PRESSURE REGULATORS, PROPELLANT TANKS, SUSTAINER ENGINES
Field(s)/Group(s):
Ground Support Systems and Facilities for Space Vehicles
Keyword(s):
ATLAS AGENA LAUNCH VEHICLES, ATLAS LAUNCH VEHICLES, RANGER SPACECRAFT, DISTRIBUTION, WEIGHT
Report Date:
1961 Sep 22