Thermo-Structural Response Caused by Structure Gap and Gap Design for Solid Rocket Motor Nozzles
Energies, 2016 The thermo-structural response of solid rocket motor nozzles is widely investigated in the design of modern rockets, and many factors related to the material properties have been considered.
Lin Sun +6 more
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Analytical investigation of solid rocket nozzle failure [PDF]
On April 5, 1983, an Inertial Upper Stage (IUS) spacecraft experienced loss of control during the burn of the second of two solid rocket motors. The anomaly investigation showed the cause to be a malfunction of the solid rocket motor. This paper presents
Hester, J., Mccoy, K. E.
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Electrical apparatus for detection of thermal decomposition of insulation Patent [PDF]
, 1971 Electrical failure detector in solid rocket propellant motor insulation against thermal degradation by fuel ...
Bernsen, B.
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Evaluation of Mono and Bimetallic Ferrocene-Based 1,2,3-Triazolyl Compounds as Burning Rate Catalysts for Solid Rocket Motor. [PDF]
ACS Omega, 2023 Valdebenito C +9 more
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Development of low cost ablative nozzles for solid propellant rocket motors, volume 1 Final report [PDF]
Evaluating low cost ablative materials for use in large solid propellant rocket ...
Laramee, R. C., Mathis, J. R.
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Reusable Solid Rocket Motor - Accomplishments, Lessons, and a Culture of Success [PDF]
, 2011 The Reusable Solid Rocket Motor represents the largest solid rocket motor ever flown and the only human rated solid motor. Each Reusable Solid Rocket Motor (RSRM) provides approximately 3-million lb of thrust to lift the integrated Space Shuttle vehicle ...
Moore, Dennis R., Phelps, Willie J.
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Measuring Fluctuating Pressure Levels and Vibration Response in a Jet Plume [PDF]
, 2011 The characterization of loads due to solid rocket motor plume impingement allows for moreaccurate analyses of components subjected to such an environment.
Knox, Douglas M., Osterholt, Douglas J.
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Solving an irregular burning problem in a small rocket motor [PDF]
Scientific Technical Review, 2014 During the design and development of a solid rocket motor, intensive irregular burning appeared in the area of high initial temperatures. The cylindrical propellant grain was designed for approximately neutral burning, with a hollow tube and both burning
Gligorijević Nikola +5 more
doaj
Optical Measurements on Solid Specimens of Solid Rocket Motor Exhaust and Solid Rocket Motor Slag [PDF]
Samples of aluminum slag were investigated to aid the Earth Science and Applications Division at the Marshall Space Flight Center (MSFC). Alumina from space motor propellant exhaust and space motor propellant slag was examined as a component of space ...
Roberts, F. E., III
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ASRM case insulation design and development [PDF]
This paper describes the achievements made on the Advanced Solid Rocket Motor (ASRM) case insulation design and development program. The ASRM case insulation system described herein protects the metal case and joints from direct radiation and hot gas ...
Bell, Matthew S., Tam, William F. S.
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