Results 81 to 90 of about 17,155 (237)
Method of igniting solid propellants Patent [PDF]
, 1966 Method for igniting solid propellant rocket motors by injecting hypergolic ...
Allen, H., Jr. +2 more
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Solid Rocket Propellant Photo-Polymerization with an In-House LED-UV Prototype. [PDF]
Polymers (Basel), 2023 Galavotti A +6 more
europepmc +1 more source
Launch vehicle performance using metallized propellants [PDF]
Metallized propellant propulsion systems are considered as replacements for the solid rocket boosters and liquid sustainer stages on the current launch vehicles: both the Space Transportation System (STS) and the Titan 4.
Palaszewski, Bryan A., Powell, Richard
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A study of the application of microwave techniques to the measurement of solid propellant burning rates Progress report, 1 Sep. 1966 - 31 Aug. 1967 [PDF]
Microwave techniques for measurement of solid rocket propellant burning ...
Obrien, W. F., Jr., Wood, H. L.
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Gimbaled, partially submerged rocket nozzle Patent [PDF]
, 1965 Gimbaled partially submerged nozzle for solid propellant rocket engines for providing directional ...
Brown, R. L.
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Technologies and New Methods for Determining the Burning Rate of Solid Propellants [PDF]
فناوری در مهندسی هوافضا, 2019 The burning rate plays animportant role in determining the performanceandballistic behavior of solid rocket propellant. In this paper, the effect of various factorson burning rate, such as combustion chamber pressure, poropellant grain initial ...
Mohammad Ali Dehnavi, Reza Emami
doaj
Numerical simulation of cook-off characteristics for AP/HTPB
Defence Technology, 2018 The present study is devoted to researching the thermal security problems of large-scale solid rocket motor with Ammonium perchlorate/Hydroxyl-terminated polybutadiene (AP/HTPB). A two-dimensional axisymmetric model for the cook-off of solid rocket motor
Qing Ye, Yong-gang Yu
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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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, 1978 A case bonded end burning solid propellant rocket motor is described. A propellant with sufficiently low modulus to avoid chamber buckling on cooling from cure and sufficiently high elongation to sustain the stresses induced without cracking is used. The
Marsh, H. E., Jr., Shafer, J. I.
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On a problem of thermo-viscoelasticity [PDF]
Analysis of viscoelastic materials under transient thermal conditions related to solid rocket ...
Knauss, W. G., Pucik, P. A.
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