Journal of Aerospace Technology and Management, 2011 The search for a smokeless propellant has encouraged scientists and engineers to look for a chlorine-free oxidizer as a substitute for AP (ammonium perchlorate).
Márcio Y. Nagamachi +3 more
doaj
The laser-induced combustion of pure ammonium perchlorate and the structure of its composite propellant flames Annual report, 16 Nov. 1968 - 15 Nov. 1969 [PDF]
Carbon dioxide laser induced combustion of pure ammonium perchlorate and structure of composite propellant ...
Hertzberg, M.
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Structural Malformations in the Neonatal Rat Brain Accompany Developmental Exposure to Ammonium Perchlorate. [PDF]
Toxics, 2023 Gilbert ME +3 more
europepmc +1 more source
A study of energy release in rocket propellants by a projectile impact method Annual report, 10 May 1967 - 9 May 1968 [PDF]
Experimental measurement of rates of energy release in solid propellants subjected to strong shock waves from projectile ...
Johns, R. H., Macek, A.
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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
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 ...
core +1 more source
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
The investigation of flame spreading over the surface of igniting solid propellants Final summary report [PDF]
Flame spreading over surface of igniting solid propellants in different gas mixtures at various ...
Magee, R. S., Mc Alevy, R. F., III
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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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