Feasibility study of a meteoroid composition analyzer spectrographic system Final report
Micrometeoroid composition determined using spectrographic analyzer to measure emission spectra of heated particles
PARTICLE MOTION↗
SEARCH · Engineering Papers
Results for “feasibility”
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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The feasibility of an orbiting 1500-meter radiotelescope
Fabrication, deployment, control, and system configuration of orbiting 1500 meter radio telescope using parabolic reflector formed by network of aluminum ribbon
RADIO TELESCOPE↗
Two hundred-sixty-in.-dia motor feasibility demonstration program. Volume V - 260-SL MOTOR chamber and nozzle shell fabrication of 18 percent-nickel maraging steel. Appendix A - Program specifications Final phase report
Procurement, process, and nondestructive test specifications for development of 260-SL motor chamber and nozzle shell fabrication of high nickel maraging steel
NOZZLE↗
Two hundred-sixty-in.-dia motor feasibility demonstration program. Volume V - 260-SL MOTOR chamber and nozzle shell fabrication of 18 percent-nickel maraging steel. Appendix C - Material characterization reports Final phase report
Chemical composition and mechanical properties of nickel maraging steel plate, forged, and weld wire materials for 260 inch diameter motor chamber and nozzle shell
MECHANICAL PROPERTY↗
Two-hundred sixty-in.-dia motor feasibility demonstration program. Volume VI - 260-SL MOTOR nozzle and exit cone assemblies. Book 1 - Text Final phase report
Design and material evaluation program for fabrication of large ablative motor nozzle and exit cone
ABLATING MATERIAL↗
A Feasibility Study on Miniaturizing an Automatic Amino Acid Analyzer for Use on Apollo Mission and Mars Voyager Mission Progress Report, Jan. - Jun. 1967
Miniaturizing n automatic amino acid analyzer for use on Apollo mission and Mars Voyager mission
AMINO ACID↗
Performance of studies to determine the feasibility of various techniques for measuring propellant mass aboard orbiting space vehicle Final report
High energy radiation methods for measuring liquid oxygen and liquid hydrogen mass in propellant tanks of orbiting spacecraft
FUEL GAUGE↗
Proceedings of NASA Conference on Supersonic-Transport Feasibility Studies and Supporting Research
Supersonic transport configurations, propulsion systems, structural materials, handling qualities, and sonic boom - conference
SUPERSONIC TRANSPORT↗
Feasibility study of a miniature solid-state pressure transducer Final report
Piezojunction effect in miniature solid state pressure transducer
SOLID STATE↗
Buoyant Venus station feasibility study. Volume II - Mode mobility studies Final report
Deployment methods using parachutes for balloon inflation, and altitude cycling for inflatable buoyant Venus station
BALLOON↗
Buoyant Venus Station feasibility study. Volume III - Instrumentation study Final report
Scientific instrumentation for inflatable buoyant Venus station
VENUS PROBE↗
Buoyant Venus station feasibility study. Volume IV - Communications and power Final report
Telecommunication and power supply requirements for inflatable buoyant Venus station
TELECOMMUNICATION↗
Buoyant Venus station feasibility study. Volume V - Technical analysis of a 200-pound BVS Final report
Compatibility of small 200-lb inflatable buoyant Venus station with Atlas Centaur launch vehicle
VENUS PROBE↗
Study on the feasibility of V/STOL concepts for short haul transport aircraft
Weight standardization, tilt and stopped rotor optimization, and noise sensitivity analysis of V/STOL concepts for short-haul transport aircraft
V/STOL↗
Assembly/sterilizer facility feasibility program, volume I Final report
Ultra-bioclean-room facility for decontamintion and sterilizion of disassembled spacecraft, and subsequent assembly and repair
CLEAN ROOM↗
A feasibility study of an experiment for determining the properties of the Mars atmosphere. Volume I - Summary
Mars probe design and subsystem performance characteristics for investigating Martian atmosphere
SPACECRAFT DESIGN↗
Feasibility of conventional control techniques for large highly coupled elastic boost vehicles Final report
Control techniques for large highly-coupled elastic boost vehicles with elastic and fuel slosh mode frequencies close to desired control frequencies - motion equations
MOTION EQUATION↗
Feasibility study for a multiple satellite system. Volume I - Summary Final report
Multiple satellites in noncoplanar array used to define spatial and temporal variations of solar wind in interplanetary space
INTERPLANETARY SPACECRAFT↗