High temperature thermocouple research and development program summary report
High temperature thermocouple research and development program - thermocouples with thermochemically formed tungsten sheath and tungsten rhenium center conductor
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High temperature thermocouple research and development program - thermocouples with thermochemically formed tungsten sheath and tungsten rhenium center conductor
Parametric determination of heat shielding requirements for manned Mars landing and return missions
Program evaluation and review technique covering progress, cost estimates, contracts, personnel panels, management and operational philosophies
Base thermal environment measured on flight tests of eight-engine LOX/RP-1 propelled Saturn I booster
IMP-I Earth satellite magnetic field measurement experimental results including solar wind flow effects
Introductory remarks to Conference on Role of Simulation in Space Technology sponsored by Virginia Polytechnic Institute in August 1964
Wind tunnel, simulator and flight test results to evaluate cockpit accelerations, handling qualities and stability and control of jet transports in severe turbulence
The studies reported herein were prepared by Lockheed Missiles & Space Company for the George C. Marshall Space Flight Center, Huntsville, Ala., under Contract No. NAS 8-5024. The results of the Early Manned Interplanetary Mission Study are reported in two volumes. Volume 1 contains the unclassified portion of the studies and Volume 2 presents the classified (CRD) studies relating to orbital escape propulsion systems.
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Space program supporting research and advanced development - systems analysis, programming, environment requirements, guidance and control, engineering mechanics, facility, and propulsion
Space exploration programs and science - Surveyor project, Mariner program, Deep Space Instrumentation Facility, space flight operation facility, environment test facility, and physics