Results 121 to 130 of about 888 (231)

Thermal Insulative Elastomers for Clustered Large Liquid Propellant Rocket Engines

open access: yes, 1964
As thrust levels increase and as rocket engines fire for longer periods of time, the difficulties encountered in the protection of critical components from the effects of excessively high temperatures greatly increase.
Peters, S. T.
core   +1 more source

COMPOSITE SOLID ROCKET PROPELLANT MATERIALS

open access: yes, 1991
Jeffrey W. Gilman, Robert D. Chapman
openaire   +2 more sources

PREPARATION AND CHARACTERIZATION OF NOVEL BINDER FOR COMPOSITE SOLID ROCKET PROPELLANT [PDF]

open access: yesThe International Conference on Chemical and Environmental Engineering, 2012
Hosam Mostafa, I. Kamal
openaire   +1 more source

High Pressure Testing Of Composite Solid Rocket Propellant Mixtures: Burner Facility Characterization

open access: yes, 2007
Much Research on composite solid propellants has been performed over the past few decades and much progress has been made, yet many of the fundamental processes are still unknown, and the development of new propellants remains highly empirical.
Carro, Rodolphe Valentin
core   +1 more source

Flexible composite membrane Patent

open access: yes, 1970
Flexible composite membrane structure impervious to extremely reactive chemicals in rocket ...
Vango, S. P., Taylor, L. L.
core   +1 more source

Microwave ignition and combustion control of 3D printed solid rocket propellant via binder additives, macro-, and micro-scale metal and metal oxides

open access: yes
Microwave irradiation offers a unique way to develop the ability to timewise actively control (throttle) solid rocket and propellant energy release.
Lajoie, Justin Andrew
core   +2 more sources

Small-scale solid rocket performance sensitivity to burn rate catalyst in ammonium perchlorate composite propellant

open access: yes
This thesis presents an analytical and experimental assessment of varying burn rate catalyst weight percentages in ammonium perchlorate composite propellant (APCP) and its effect on solid rocket motor performance.
Besmer, Caleb
core  

SIC/SIC composite thruster for a non-toxic liquid propellant rocket engine

open access: yes, 2017
Combustion chamber and nozzle for a non-toxic liquid rocket engine made by Tyrano ZMI SiC fiber reinforced SiC matrix composite were tested under sea level combustion tests.
Tokudome, Shinichiro   +2 more
core   +1 more source

Investigation of the characteristics of rocket solid propellant sample by experimentally

open access: yes, 2018
Sunulan tez çalışması ile numune kompozit katı roket yakıtının karakteristik özelliklerinin belirlenmesi için deneysel çalışmalar yapılmıştır. Katı roket yakıtlarında roket performansını belirleyen en önemli faktörlerden biri yanma hızıdır.
Dönmez, Can Emre
core  

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