Development of an environmentally immune electrostatic insensitive Apollo standard initiator Final report
Improved electrostatic discharge protection for Apollo standard initiator under deep space conditions
APOLLO PROJECT↗
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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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Design and fabrication of a trace contaminant removal system for Apollo, phase III Final report, Sep. 1965 - Feb. 1966
Sorbent material and platinum and palladium catalyst testing for development of Apollo spacecraft trace contaminant removal system
APOLLO SPACECRAFT↗
Study to determine an improved method for Apollo propellant system decontamination and propellant tank drying, phase I Interim report
Improve method for Apollo propellant system decontamination and propellant tank drying
APOLLO PROJECT↗
Structural and dynamic analysis of the Apollo AFT heat shield Final report, Sep. 12, 1964 - Mar. 1, 1966
Structural and dynamic analysis of Apollo aft heat shield
STRUCTURAL DYNAMICS↗
Development of passive temperature control coatings for use on the Apollo vehicle ablative thermal protection system Final report
Passive temperature control coatings for Apollo spacecraft ablative thermal protection system
TEMPERATURE CONTROL↗
Apollo Unified S-Band System
Unified S-band telecommunication system for Apollo spacecraft-ground station communications
APOLLO PROJECT↗
Manual control of high-altitude Apollo launch abort
Simulation study of manual control capability for Apollo spacecraft reentry orientation after high altitude launch abort using visual scene
REENTRY↗
Spacecraft capability for Apollo scientific experiments
Containers, storage compartments, and weight and volume distributions of scientific payloads aboard Apollo spacecraft for lunar exploration
APOLLO SPACECRAFT↗
Apollo LEM adapter structural analysis Final report, Jan. 1965 - Apr. 1966
Stress and deformation analysis for Apollo lunar excursion module adapter under mechanical and thermal loading
DEFORMATION↗
The Apollo Unified S-Band System
Unified S-band system for tracking and communicating with Apollo spacecraft during lunar mission
APOLLO SPACECRAFT↗
Apollo Spacecraft Gaseous Nitrogen Deluge System
System requirements, design data, and cost estimates for Apollo spacecraft gaseous nitrogen deluge system
GAS TRANSPORT↗
Infrared Sensor for Apollo Reentry Final Report, 1 Jul. - 30 Dec. 1964
Infrared sensor used to augment radio frequency tracking during Apollo vehicle reentry into earth atmosphere
RADIO FREQUENCY↗
Operation, maintenance and data, Apollo docking test device, AMF part no. 359-60001 Technical manual
Operation and maintenance manual for test device for simulation of Apollo mission docking maneuvers
FLIGHT SIMULATION↗
Feasibility study of constructing a 1/10 scale Apollo service module similitude model Final report
Feasibility of constructing scale model of Apollo service module to measure effects of aerodynamic fluctuating pressures generated during boost flight
SCALE MODEL↗
Proceedings of the experimenters' information meeting on the Apollo Applications Program in bioscience
Experimenters conference on Apollo Applications Program in biological sciences
EXPERIMENT DESIGN↗
A system for re-entry tracking of the Apollo spacecraft
Wide beam radio interferometer system for reentry tracking of Apollo spacecraft
APOLLO SPACECRAFT↗
Pressurization system for use in the Apollo service propulsion system Interim report
Fuel tank pressurization for use in Apollo service propulsion system
FUEL TANK PRESSURIZATION SYSTEM↗
Experimental rocket performance of Apollo storable propellants in engines with large area ratio nozzles
Nitrogen tetroxide and blend of hydrazine and unsymmetrical dimethyl hydrazine evaluated in rocket engines with large area ratio nozzles - Apollo project
STORABLE PROPELLANT↗