Electrostatically driven capacitor project final technical report
Electrostatically driven capacitor with drive circuitry for electrometer applications in space instrumentation
SPACECRAFT INSTRUMENTATION↗
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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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Testing and evaluation of nickel-cadmium spacecraft-type cells final technical report
Testing and evaluation of nickel-cadmium cells - vibration, shock, acceleration, and life cycle tests
NICKEL-CADMIUM BATTERY↗
Analysis of the project fire re-entry package flow field final technical report
Theoretical prediction of state of gas in flow field surrounding Apollo type vehicle in reentry at hypersonic speeds
GAS FLOW↗
The development of a cesium-vapor-filled thermionic energy converter final technical report, 18 jun. - 18 nov. 1962
Cesium-vapor-filled thermionic energy converter for solar heat application
CESIUM VAPOR↗
Adhesion and cohesion of metals Final technical report, 24 Mar. 1964 - 1 Jan. 1965
Adhesion and cohesion of metals for use in components of electrical and mechanical devices required for space exploration
ADHESION↗
A study of solid-propellant vaporization and diffusion processes Final technical report
Vaporization rate and diffusion coefficient determined for organic additives to polyurethane solid propellants - dioctyl adipate and ferrocene
SOLID PROPELLANT↗
Surveyor Lunar Roving Vehicle, phase I. Volume V - System evaluation Final technical report
Surveyor Lunar Roving Vehicle /SLRV/ mission in support of Apollo LEM program
MISSION PLANNING↗
Surveyor Lunar Roving Vehicle, phase I. Volume III - Preliminary design and system description. Book I - System description and performance characteristics Final technical report
Surveyor Lunar Roving Vehicle /SLRV/ system description and performance characteristics
SYSTEMS ANALYSIS↗
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↗
Development of a second generation prototype reflectometer for reflectance measurement in space Final technical report
Prototype reflectometer development for reflection measurements in space
MEASURING APPARATUS↗
Balloon Experiments with the STL Flight Prototype Luminescent Chamber Final Technical Report
Performance of flight prototype luminescent chamber during high altitude balloon flight
BALLOON FLIGHT↗
Juncture stress fields in multicellular shell structures. Volume VIII - Buckling analysis of segmental orthotropic cylinders under non-uniform stress distribution Final technical report
Orthotropic cylindrical shell buckling under axial compression - structural dynamics
STRUCTURAL DYNAMICS↗
The development of a cesium-vapor-filled thermionic energy converter Final technical report
Cesium-vapor-filled thermionic energy converter design, fabrication, and testing
CESIUM VAPOR↗
Surveyor Lunar Roving Vehicle, interim study Final technical report
Remote control study of Surveyor Lunar Roving Vehicle /SLRV/ test model
LUNAR ROVING VEHICLE /LRV/↗
Application of gyrocompassing to space missions Final technical report
Gyrocompassing with sensors or inertial platforms for use on planetary surface or in free orbital flight
INERTIAL PLATFORM↗
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↗