Scale 1/14.2 investigation of submerged nozzle for SL-3 260-inch solid rocket
Submerged nozzle design for SL-3 260-inch solid propellant rocket engines
Pelouch, J. J., Jr.↗
SEARCH · Search NASA
Results for “Solid propellant rocket engine”
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Compilation of rocket spin data. Volume 1 - Acceleration test facilities Final report
Spin and centrifuge test facilities for testing solid rocket propellant engines - annotated bibliography
Manda, L. J.↗
Stress analysis of solid propellant rocket motors
Linear viscoelastic and elastic problem in stress analysis of solid propellant rocket engines
Akyuz, F. A.↗
Compilation of rocket spin data. Volume 2 - Literature survey Final report, Nov. 1966 - Aug. 1968
Literature survey of acceleration spin effects on solid propellant rocket engines
Manda, L. J.↗
Compilation of rocket spin data. Volume 3 - Data evaluation and recommendations Final report, Nov. 1964 - Aug. 1968
Qualitative analysis of spin acceleration effects on solid propellant rocket engine performance
Manda, L. J.↗
Development of a thermal barrier coating for use on a water-cooled nozzle of a solid propellant rocket motor Final report
Thermal barrier coating for use on water cooled nozzle of solid propellant rocket engine
Stubbs, V. R.↗
A comparison of experimental heat-transfer coefficients in a nozzle with analytical predictions from Bartz's methods for various combustion chamber pressures in a solid propellant rocket motor
Comparison of experimental heat transfer coefficients in a nozzle with analytical predictions for various combustion chamber pressures in solid rocket propellant engine
Smith, D. M.↗
Development of microwave NDT inspection techniques for large solid propellant rocket motors Final report
Microwave nondestructive testing techniques for large solid propellant rocket engines
Eckert, T. E.↗
The Applications Technology Satellite apogee rocket motor - A summary report
Design, testing, and development of solid propellant rocket engine for orbital transfer of Applications Technology Satellite
Anderson, R. G.↗
An application of the requirement vs capability analysis to estimating design reliability of solid rocket motors
Design reliability parameters for solid propellant rocket engines
Hermann, C. R.↗
Spherical solid-propellant rocket motor Patent
Spherical solid propellant rocket engine design
Styles, C. M.↗
Gimbaled, partially submerged rocket nozzle Patent
Gimbaled partially submerged nozzle for solid propellant rocket engines for providing directional control
Brown, R. L.↗
Spherically-shaped rocket motor Patent
Spherical solid propellant rocket engine having abrupt burnout
Odonnell, T. J.↗
Propellant grain for rocket motors Patent
Grain configuration for solid propellant rocket engines
Pierce, R. M.↗
Demonstration of a sterilizable solid propellant rocket motor Final report, Feb. 1969 - Jul. 1970
Demonstration of solid propellant rocket engine for unmanned planetary landers to withstand dry heat sterilization
Weinberg, L.↗
Design, fabrication, and test of omnidirectional flexible seals for thrust vector control of large solid rocket motors Final report
Omnidirectional flexible, rubber-steel seal design, fabrication, and performance testing for solid propellant rocket engine thrust vector control
Wong, E. Y.↗
Design criteria monograph for pressurized metal cases
Organiation and presentation of data pertaining to design of solid propellant rocket engine cases are discussed. Design criteria are presented in form of monograph based on accumulated experience and knowledge. Improvements in reliability, cost effectiveness, and engine efficiency are stressed.
Source record↗
Study of solid rocket motor for a space shuttle booster. Appendix A: SRM water entry loads
An analysis of the water entry loads imposed on the reusable solid propellant rocket engine of the space shuttle following parachute descent is presented. The cases discussed are vertical motion, horizontal motion, and motion after penetration. Mathematical models, diagrams, and charts are included to support the theoretical considerations.
Source record↗