Performance of rocket nozzle materials with several solid propellants [PDF]
Erosion resistance and thermal stress cracking tests of rocket nozzle materials with solid ...
Freche, J. C. +2 more
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Chemically Collapsible Mandrel for Solid Rocket Motor Processing
Journal of Aerospace Technology and Management, 2015 Composite propellant mainly consists of two parts, binder matrix (prepolymer, plasticizer, cross linker, antioxidant and curative etc.) and solid ingredients (oxidizer, metal fuel, burn rate modifier, combustion stabilizer etc.).
Abhijit Dey +3 more
doaj
Next generation earth-to-orbit space transportation systems: Unmanned vehicles and liquid/hybrid boosters [PDF]
The United States civil space effort when viewed from a launch vehicle perspective tends to categorize into pre-Shuttle and Shuttle eras. The pre-Shuttle era consisted of expendable launch vehicles where a broad set of capabilities were matured in a ...
Hueter, Uwe
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Study on Rheological Properties and Pouring Process of Hydroxyl-Terminated Polybutadiene (HTPB) Propellants. [PDF]
Polymers (Basel), 2023 Wang H, Ji Y, Jiang X, Li Z.
europepmc +1 more source
Propulsion simulation for magnetically suspended wind tunnel models [PDF]
The feasibility of simulating propulsion-induced aerodynamic effects on scaled aircraft models in wind tunnels employing Magnetic Suspension and Balance Systems. The investigation concerned itself with techniques of generating exhaust jets of appropriate
Beerman, Henry P. +5 more
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Space station propulsion: The advanced development program at Lewis [PDF]
A reference configuration was established for the initial operating capability (IOC) station. The reference configuration has assumed hydrazine fueled thrusters as the propulsion system.
Jones, R. E.
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Preliminary performance and life evaluations of a 2-kW arcjet [PDF]
The first results of a program to expand the operational envelope of low-power arcjets to higher specific impulse and power levels are presented. The performance of a kW-class laboratory model arcjet thruster was characterized at three mass flow rates of
Curran, Francis M., Morren, W. Earl
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Advances in Structural Reliability Analysis of Solid Propellant Grain: A Comprehensive Review. [PDF]
Polymers (Basel)Tang C +4 more
europepmc +1 more source
Three-dimensional finite element analysis of acoustic instability of solid propellant rocket motors [PDF]
A three dimensional finite element solution of the acoustic vibration problem in a solid propellant rocket motor is presented. The solution yields the natural circular frequencies of vibration and the corresponding acoustic pressure mode shapes ...
Hackett, R. M., Juruf, R. S.
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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