Sampling with a luster sounding rocket during a Leonid meteor shower.
Micrometeoroid sampling with Luster sounding rocket during Leonid meteor shower, detailing contamination control program
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Micrometeoroid sampling with Luster sounding rocket during Leonid meteor shower, detailing contamination control program
Flight strain gauge system for Centaur /AC-6/ LIQUID hydrogen fuel tank skin
Synthesis of formaldehyde by oxidation of methane
Oxidation of methane to formaldehyde in reactors coated with potassium tetraborate
Deployment characteristics of dynamic and elastic parawing scale model for spacecraft recovery
Separation and identification of contaminants found on collecting surfaces exposed to Leonid meteoroid shower in 1965
Supersonic transport design and requirements for sonic boom reduction
Micrometeoroid penetration of metal thin film on Gemini 9 and 12, finding no evidence of impact
Extraterrestrial dust particle data from sounding rocket flights and manned satellites, discussing particle size distribution and meteoritic composition
Particle concentrations and size distribution on Luster sounding rocket surfaces exposed to Leonid meteroid shower, comparing contamination and extraterrestrial origins
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Sonic boom signatures produced by diverse SST configurations during cruise, indicating aircraft length as overpressure limit factor
Modified supersonic turbine cycle provides cooling air to surrounding structures. Simplified mechanical design assures correct balance of air flow, allows direct issue of cool air to the structure, and assists in matching turbine work output to work input required by the compressor.
Test lead wire attachment quickly and securely engages screw head by expansion against the side walls of the screw head slot. Heat shrinkable tubing is used for the forward and shaft ends to insulate the device from accidental contact.
Turbine-compressor system for active cooling of hypersonic aircraft
Microparticle collection experiments during 1966 Orionid and Leonid meteor showers accomplished by Luster and ALARR /air launched-air recovered rocket/ instruments
SST configurations minimizing sonic booms obtainable for given length and weight
Economic impact of modifications to DC-8 aircraft nacelles to reduce fan-compressor noise - Part 5