Feasibility of obtaining hypervelocity acceleration using propellant lined launch tubes Final report, 27 Sep. 1966 - 5 May 1970 [PDF]
Feasibility of explosive lining in launch tube for hypervelocity projectile ...
Rodenberger, C. +2 more
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Addition of solid oxidizer increases liquid fuel specific impulse [PDF]
, 1967 Adding soluble solid oxidizers to hydrazine and similar fuels makes them useful in low temperature bipropellant systems. These oxidizers improve the low specific impulse, high freezing point, low boiling point, and low density of the ...
Hendel, F. J.
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Possibility of aluminium/magnesium exchange in composite rocket propellants [PDF]
Scientific Technical Review, 2018 Composite solid propellants based on ammonium perchlorate/hydroxyterminated polybutadiene/isophorone dyisocyanate including two metal components: aluminium and magnesium with different contents have been represented in this paper.
Rodić Vesna +3 more
doaj
Journal of Aerospace Technology and Management, 2013 http://dx.doi.org/10.5028/jatm.v5i2.229 The research for low toxicity and no damage to the environment has stimulated the development of specific investigation lines in many areas.
Gilson da Silva +2 more
doaj
Development, qualification, and delivery of a hydrogen burnoff igniter [PDF]
The hydrogen burnoff igniter, a pyrotechnic device used to burn off excess hydrogen gas near the Space Shuttle Main Engine (SSME) nozzle, was designed, fabricated, and qualified.
Ray, D.
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Analysis of quasi-hybrid solid rocket booster concepts for advanced earth-to-orbit vehicles [PDF]
A study was conducted to assess the feasibility of quasi-hybrid solid rocket boosters for advanced Earth-to-orbit vehicles. Thermochemical calculations were conducted to determine the effect of liquid hydrogen addition, solids composition change plus ...
Andreev T. +7 more
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The Role of Boron in Thermal Decomposition of Ammonium Perchlorate [PDF]
Iranian Journal of Chemistry & Chemical Engineering, 2000 Simultaneous thermal analysis (STA) method has been applied to study decomposition reactions of AP under a flowing nitrogen atmosphere and static air.
Abdolsamad Zarrin Ghalam Moghaddam +1 more
doaj
Enhanced Catalytic Effect of Ti2CTx-MXene on Thermal Decomposition Behavior of Ammonium Perchlorate. [PDF]
Materials (Basel), 2022 Li J, Du Y, Wang X, Zhi X.
europepmc +1 more source
Heat-sterilizable, remotely activated battery development program, phase 1 Quarterly report, 1 Jul. - 30 Sep. 1968 [PDF]
Testing of absorbent plate separation materials and propellant formulations to characterize battery components ability to withstand dry heat ...
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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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