Apollo experiments support on preliminary estimate of development costs and schedule for molab task report
Preliminary development cost estimate for Apollo project lunar mobile laboratory /Molab/
COST ESTIMATE↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Command system study for the operation and control of unmanned scientific satellites. task i- unified tracking/command/telemetry at lunar distances first quarterly progress report, 30 jun. - 30 sep. 1964
Control of unmanned scientific satellites and unified tracking/command/telemetry at lunar distances
TELEMETRY↗
Investigation of a manual sextant-sighting task in the ames midcourse navigation and guidance simulator
Midcourse simulator analysis of manual sextant sighting for interplanetary navigation
INTERPLANETARY NAVIGATION↗
Command system study for the operation and control of unmanned scientific satellites. task ii closed-loop /feedback/ verification techniques second quarterly progress report, 30 sep. - 31 dec. 1964
Closed loop, feedback verification techniques for command system of unmanned scientific satellite
FEEDBACK CONTROL SYSTEM↗
Solar energy thermionic /set/ program, task ii final report, 27 oct. 1963 - 18 dec. 1964
Advanced converter structure capable of satisfying geometrical constraints of generator designs for Solar Energy Thermionic /SET/ PROGRAM
SOLAR ENERGY THERMIONIC /SET/ PROGRAM↗
Task iv- /research/ of the solar energy thermionic /set/ conversion development program third quarterly progress report, 1 dec. 1964 - 28 feb. 1965
Operational parameters for thermionic converter - cesium vapor diode formulation and computer method of analysis
THERMIONIC CONVERTER↗
Research on utilization of part task spatial orientation information in the dynamic simulator
Error and control efficiency analysis of pilots exposed to simulated pitch, roll, yaw, and altitude variations
PILOT PERFORMANCE↗
Command system study for the operation and control of unmanned scientific satellites, task III - Command system interference Third quarterly progress report, 1 Jan. - 31 Mar. 1965
Effects of CW and modulated interference on baseband of AM and FM demodulators used for control of unmanned scientific satellites
SATELLITE CONTROL↗
Voyager spacecraft. Volume I - Preferred design - System considerations Final technical report, phase IA, task B
Voyager spacecraft preferred design
SPACECRAFT DESIGN↗
Voyager spacecraft. Volume II - Preferred design - Subsystems Final technical report, phase IA, task B
Preferred design for Voyager spacecraft subsystems
SYSTEMS DESIGN↗
Voyager spacecraft. Volume III - Spacecraft implementation Final technical report, phase IA, task B
Voyager spacecraft implementation plan
PLANNING↗
Voyager spacecraft. Volume IV - Operational support equipment Final technical report, phase IA task B
Operational support equipment for Voyager spacecraft
VOYAGER PROJECT↗
Voyager spacecraft. Volume V - Tradeoff analyses Final technical report, phase IA, TASK B
Tradeoff analyses for Voyager spacecraft propulsion system selection
VOYAGER PROJECT↗
Voyager spacecraft system. Volume A - Preferred design for flight spacecraft and hardware subsystems, part I Final technical report, task B
Scientific investigation of solar system with instrumented, unmanned spacecraft to fly, orbit and land on planets - Voyager project
PLANETARY ORBIT↗
Voyager spacecraft system. Volume A - Preferred design for flight spacecraft and hardware subsystems, part II Final technical report, task B
Hardware subsystems for flight spacecraft, design reliability, interface control, and mission objectives - Voyager project
SUBSYSTEM↗
Voyager spacecraft system. Volume B - Design for the operational support equipment Final technical report, task B
Operational support equipment for Voyager flight spacecraft
TEST EQUIPMENT↗
Voyager spacecraft system. Volume C - Alternate designs considered for spacecraft propulsion systems Final technical report, task B
Solid-liquid systems sized for 1971 and 1973 missions and 1975 and 1977 missions, Apollo lunar excursion module descent propulsion system, and Titan III-C transtage
LIQUID PROPELLANT↗
Voyager spacecraft system - Phase IA, TASK B, preliminary design. Spacecraft functional description, volume A
Mission objectives and systems design criteria for 1971 Voyager spacecraft concept
SYSTEMS DESIGN↗