Results 71 to 80 of about 31,065 (215)

A Nonlinear Viscoelastic Constitutive Model for Solid Propellant with Rate-Dependent Cumulative Damage. [PDF]

Materials (Basel), 2022
Chen S, Wang C, Zhang K, Lu X, Li Q.
europepmc   +1 more source

C/C-SiC Composites for Nozzle of Solid Propellant Ramjet

Journal of Aeronautical Materials, 2017
Carbon fiber reinforced carbon and silicon carbide matrix composites for nozzle inner of solid propellant ramjet were prepared by using the hybrid process of "chemical vapor infiltration + precursor impregnation pyrolysis (CVI+PIP)".
WANG Lingling, JI Alin, GAO Yaqi, CUI Hong, YAN Liansheng, PANG Fei   +5 more
doaj   +1 more source

Preparation and Properties of a Novel High-Toughness Solid Propellant Adhesive System Based on Glycidyl Azide Polymer-Energetic Thermoplastic Elastomer/Nitrocellulose/Butyl Nitrate Ethyl Nitramine. [PDF]

Polymers (Basel), 2023
Zhang J, Wang Z, Sun S, Luo Y.
europepmc   +1 more source

Launch vehicle performance using metallized propellants [PDF]

Metallized propellant propulsion systems are considered as replacements for the solid rocket boosters and liquid sustainer stages on the current launch vehicles: both the Space Transportation System (STS) and the Titan 4.
Palaszewski, Bryan A., Powell, Richard
core   +1 more source

Development of high burn rate propellant and testing in miniature rocket motor for control applications

FirePhysChem
For aerospace vehicles, notably missiles or satellites for attitude and divert control, impulsive thrusters are most desirable if they are quantized as exact instantaneous pulses available over and after extended periods of inactive storage.
Y. Raj Alexander, Nikunj Rathi, P.A. Ramakrishna   +2 more
doaj   +1 more source

Possible meteoroid hazard to solid- propellant rocket motors [PDF]

Meteoroid hazards to solid propellant rocket ...
Robillard, C. L.
core   +1 more source

Solid rocket technology advancements for space tug and IUS applications [PDF]

In order for the shuttle tug or interim upper stage (IUS) to capture all the missions in the current mission model for the tug and the IUS, an auxiliary or kick stage, using a solid propellant rocket motor, is required.
Ascher, W., Bailey, R. L., Behm, J. W., Gin, W.   +3 more
core   +1 more source

Composite solid propellant flame microstructure determination Annual report, 23 Jun. 1967 - 22 Jun. 1968 [PDF]

Composite solid propellant flame microstructure ...
Friedman, R., Hertzberg, M., Mc Hale, E. T., Von Elbe, G.   +3 more
core   +1 more source

An experimental study on the erosion of solid propellant by cavitation water jet in submerged environment

Polymer Testing
The submerged cavitation water jet (SCWJ) is a promising technology for removing solid propellant from old solid rocket engines and recycling them. In this study, the feasibility of using SCWJ to break solid propellant is investigated.
Wenjun Zhou, Bo Liu, Meng Zhao, Xuanjun Wang   +3 more
doaj   +1 more source

Effects of propellant composition variables on acceleration-induced burning-rate augmentation of solid propellants [PDF]

This work was conducted to define further the effects of propellant composition variables on the acceleration-induced burning rate augmentation of solid propellants.
Northam, G. B.
core   +1 more source