Aimp summary description
Radiation, passive, magnetometer, meteorite flux, and solar-cell damage experiments by lunar- anchored satellite
LUNAR SATELLITE↗
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Results for “Description”
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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Apollo digital up-data link description
Digital updata link equipment used on Apollo command module
COMMAND MODULE↗
Functional description of unified s-band system and integration into the manned space flight network
Apollo unified S-band communications system and integration into manned space flight network
MANNED SPACE FLIGHT↗
Description and results of tests performed at Fucino Earth Station with Relay I
Communications and tracking facilities of Fucino ground station in Italy, and experiments conducted with Relay I satellite
COMMUNICATION SYSTEM↗
A imp mission profile and real time computing system description
Anchored interplanetary monitoring platform /IMP/ SATELLITE mission events and real time computing system support
INTERPLANETARY SPACECRAFT↗
Surveyor lunar roving vehicle, phase I. Volume III - Preliminary design and system description. Book 2 - Validation of preliminary design, sections 7-13 Final technical report
Systems design validation of Surveyor lunar roving vehicle - navigation, control and display, television, telecommunications, power supply, and thermal control
SURVEYOR PROJECT↗
Description of Langley low-frequency noise facility and study of human response to noise frequencies below 50 cps
Test facility for determining human performance in very low frequency noise environment - physiological and psychological responses
PSYCHOLOGICAL EFFECT↗
Surveyor lunar roving vehicle, phase I. Volume III - Preliminary design and system description. Book 2 - Validation of preliminary design Final report
Validation of preliminary design for Surveyor lunar roving vehicle - mobility, structure, deployment, folding and erection mechanism, and Apollo support scientific experiments
SURVEYOR PROJECT↗
Coating selection program. Part II - Program description and user's manual Final report
Computer program to select optical coating pattern for controlling temperature of spacecraft external surface
COMPUTER PROGRAM↗
Ranger VIII and IX. Part I - Mission description and performance
Ranger VIII and Ranger IX mission - pre-launch and launch operations, Atlas Agena launch vehicle system, deep space network, flight path, flight operations, and spacecraft subsystems
ATLAS AGENA LAUNCH VEHICLE↗
Summary description of a method of optimizing camber surfaces for wing-body combinations at supersonic speeds
Digital computer program using influence coefficients method for optimizing camber surfaces for wing-body combinations at supersonic speeds
WING BODY↗
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↗
Physical parameters instrumentation for surveyor interface and descriptive information
Surveyor instrumentation for measuring physical parameters on and beneath lunar surface
LUNAR SURFACE↗
Description and analysis of 890-MHz noise-measuring equipment
Ranger spacecraft noise measuring equipment for subsystem interference with spacecraft receiver
NOISE MEASUREMENT↗
Visibility in space - Target description subroutine
Computer subroutine for use in calculating visibility of Lunar Excursion Module /LEM/ ASCENT stage during moon orbit rendezvous with Command Service Module /CSM/
COMPUTER METHOD↗
Prediction of the dynamic environment of spacecraft components. Part I - General concepts and description of computer programs Technical report no. 5
Motion in spacecraft response and computer methods and programs for computing structural and air path response
DYNAMIC RESPONSE↗
Apollo mission description
This paper describes a typical Apollo lunar landing mission. The particular example chosen provides a 24-hour stay on the lunar surface and has a total duration of slightly more than eight days.
LANDING SITE↗
Spacecraft description
Command, service, and excursion modules of lunar exploration spacecraft, and communication links with earth stations
SERVICE MODULE↗