Results 131 to 140 of about 7,758 (239)

Composite Solid Rocket Propellant Aging: Multi Parameter Statistical Analysis

open access: yesInternational Journal of Aeronautics and Aerospace Engineering, 2022
openaire   +1 more source

Ice nucleus activity measurements of solid rocket motor exhaust particles [PDF]

open access: yes
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.
core   +1 more source

Nano-Iron as a Catalyst in Isocyanate-Free Rocket Propellants. [PDF]

open access: yesPolymers (Basel)
Chmielarek M   +2 more
europepmc   +1 more source

Study on Composite Solid Propellants for Rocket Assisted Projectile

open access: yesJournal of the Korean Society for Aeronautical & Space Sciences, 2010
Kyung-Moo Kim   +2 more
openaire   +2 more sources

Development of a computerized analysis for solid propellant combustion instability with turbulence [PDF]

open access: yes
A multi-dimensional numerical model has been developed for the unsteady state oscillatory combustion of solid propellants subject to acoustic pressure disturbances.
Chung, T. J., Park, O. Y.
core   +1 more source

Hybrid propulsion technology program. Volume 1: Conceptional design package [PDF]

open access: yes
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
core   +1 more source

Thermal Insulation Based on NBR-Elastomerized Phenolic Resin Reinforced with Carbon Fibers: Mechanical and Ablation Properties. [PDF]

open access: yesMaterials (Basel)
Gržetić J   +6 more
europepmc   +1 more source

Identification and management of filament-wound case stiffness parameters [PDF]

open access: yes
The high specific strength and the high specific modules made graphite epoxy laminate an expedient material substitute for the Shuttle Solid Rocket Motor steel case to substantially increase the payload performance without increasing the composite case ...
Rheinfurth, M., Verderaime, V.
core   +1 more source

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