HISTORY OF THE CLUSTER SYSTEM
Space science - solid propellant rocket clusters for satellite carrier systems
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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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Space science - solid propellant rocket clusters for satellite carrier systems
Fitting solid propellant rocket engine into space vehicle design
Short duration technique providing simulation of thermodynamic properties and composition of exhaust products of liquid and solid propellant rocket engines
Spectrophotometric method for measurement of aluminum oxide particle sizes during burning of solid propellant rocket engine
Fluid controlled solid rocket motor using fully oxidized solid propellant grain configured with oversized nozzle throat area
Radio-attenuation measurement /ram a1/ test, four- stage solid-propellant rocket vehicle - performance and design
Hydrotest failure analysis of arc welded, solid propellant rocket motor case
Auxiliary solid propellant motors in Saturn launch vehicle
Rocket chamber pressure influence on particle size measurements of heterogeneous combustion products of solid propellants containing aluminum
Carbon phenolic, graphite phenolic, and silica phenolic nozzle ablative materials performance for large solid propellant rocket boosters
Third 260-inch diameter solid propellant rocket engine test firing
Necessity of vehicle and motor designers of solid- propellant motors to consider upper stage, performance and thrust vector control requirements
Solid propellants and motors for space exploration, comparing chemical and nonchemical propulsion systems
Heat and mass transfer characteristics of liquid film cooling, optimum thrust nozzle contours, liquid propellant combustion processes and ignition of solid propellants
Conceptual design of half-size multipurpose large launch vehicle with liquid propellant main and injection stages and solid propellant strap-on stage
This volume is a compilation of 48 unclassified/unlimited distribution papers presented at the 1997 meeting of the JANNAF 34th Combustion Subcommittee (CS) held jointly with the Propulsion Systems Hazards Subcommittee (PSHS), and the Airbreathing Propulsion Subcommittee. Proceedings of the CS, PSHS and APS meetings are published separately by CPIA. The CS Meeting Proceedings are published in four volumes. The JANNAF papers contained in this volume contributed to the Second Year Progress Review of the Multidisciplinary University Research Initiative Program (MURI) on 'Novel New Ingredients to Stabilize Rocket Motors'. Technical progress made on this program was presented as JANNAF CS papers contained in Volumes 2 and 4. Papers contained in this volume review bi-plateau propellant combustion, AP and metal combustion, solid propellant combustion instability fundamentals and motor applications, gas-phase and condensed-phase kinetics, and measurement techniques.
Flight tests of solid propellant rockets in dynamic spin or roll environments
Applications Technology Satellite solid propellant apogee motor qualification tests