Solid Rocket Motor Metal Cases
Guidelines and practices for design of solid rocket motor cases
Source record↗
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Results for “casing”
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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On the integrability cases of the equation of motion for a satellite in an axially symmetric gravitational field
Integrability cases of equation of motion for satellite in axially symmetric gravitational field
Ghaffari, A.↗
Mandrel for shaping solid propellant rocket fuel into a motor casing Patent
Mandrel for shaping solid propellant rocket fuel into engine casing
Lewis, D. J.↗
Some observations of effects of porous casings on operating range of a single axial-flow compressor rotor
Test results of single axial flow with several porous outer casings
Bailey, E. E.↗
Stresses in case-bonded solid-propellent rocket motors under transverse body-force loading
Two dimensional plane stress photoelastic models of star configurations in elastic case bonded solid propellant rocket motors under transverse body force loading
Parmerter, R. R.↗
Forced transverse vibration of a solid viscoelastic cylinder bonded to a thin casing
Solid viscoelastic cylinder bonded to thin elastic casing, analyzing normal and tangential stresses for stress and displacement frequency responses in forced transverse vibration
Sann, R. I.↗
An analysis of adhesive debonding in case-bonded solid propellant rocket motors
Adhesive debonding in case-bonded solid propellant rocket motors, describing stress analysis and interfacial surface energy measurement
Kunio, T.↗
Non-magnetic battery case Patent
Nonmagnetic hermetically sealed battery case made of epoxy resin and woven glass tape for use with electrochemical cells in spacecraft
Hennigan, T. J.↗
Method of making a rocket motor casing Patent
Method for shaping regeneratively cooled rocket motor casing having minimum thickness at each channel cross section
Baehr, E. F.↗
Rocket motor casing Patent
Regeneratively cooled rocket motor casing with tapered channels to insure minimum thicknesses at each channel cross section for necessary strength requirements
Baehr, E. F.↗
Payload/burned-out motor case separation system Patent
Payload/spent rocket engine case separation system
Watson, N. D.↗
Ion engine casing construction and method of making same Patent
Permanently magnetized ion engine casing construction for use in spacecraft propulsion systems
Sohl, G.↗
Sealed electrochemical cell provided with a flexible casing Patent
Sealed electrochemical cell with flexible casing for varying electrolyte level in cell
Hennigan, T. J.↗
Task 4 stage data and performance report for casing treatment investigations. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 1
Test description and results for high Mach number transonic fan stages to determine range and distortion tolerance for various rotor tip casing treatment configurations
Tesch, W. A.↗
Task 4 stage data and performance report for casing treatment investigations. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 2
Tabulations of blade element and circumferential distortion flow data in tests of high Mach number transonic fan stages with various rotor tip casing treatment configurations
Tesch, W. A.↗
Formulating propellants for fully case-bonded end-burning motors
Low modulus solid propellants family for low thrust-to-mass ratio fully case bonded end-burning motors, using polymer network theory for binder formulation
Marsh, H. E., Jr.↗
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.
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Effects of casing boundary-layer removal on noise of a turbofan rotor
The effect of casing boundary-layer removal on noise produced by a turbofan rotor was measured. The outlet guide vanes were removed for these tests. A comparison was made between the noise measurements when the boundary layer was bled off and under zero bleed conditions. When the boundary layer was removed, overall sound pressure level was reduced 2 dB with moderate blade loading and 3 dB with heavier blade loading. An analysis of the changes in the spectral density with bleed is presented.
Goldstein, A. W.↗