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
Study on Mechanical Properties and Failure Mechanisms of Highly Filled Hydroxy-Terminated Polybutadiene Propellant under Different Tensile Loading Conditions. [PDF]
Polymers (Basel), 2023 Wu C +6 more
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Ice nucleus activity measurements of solid rocket motor exhaust particles [PDF]
The ice Nucleus activity of exhaust particles generated from combustion of Space Shuttle propellant in small rocket motors has been measured. The activity at -20 C was substantially lower than that of aerosols generated by unpressurized combustion of ...
Keller, V. W.
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Qualification Phase for the Applications Technology Satellite Apogee Rocket Motor Technical Memorandum, Jul. - Aug. 1966 [PDF]
Qualifications tests on applications technology satellite apogee rocket motor ...
Anderson, R. G., Frank, D. R.
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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
A design study of hydrazine and biowaste resistojets [PDF]
A generalized modeling program was adapted in BASIC on a personal computer to compare the performance of four types of biowaste resistojets and two types of hydrazine augmenters. Analyzed biowaste design types were: (1) an electrically conductive ceramic
Barker, L., Page, R. J., Stoner, W. A.
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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
Hybrid propulsion technology program. Volume 1: Conceptional design package [PDF]
A concept design study was performed to configure two sizes of hybrid boosters; one which duplicates the advanced shuttle rocket motor vacuum thrust time curve and a smaller, quarter thrust level booster.
Holzman, Allen L. +5 more
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Nano-Iron as a Catalyst in Isocyanate-Free Rocket Propellants. [PDF]
Polymers (Basel)Chmielarek M +2 more
europepmc +1 more source
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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