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A solid-propellant rocket or solid rocket is a rocket with a rocket engine that uses solid propellants (fuel/oxidizer). The earliest rockets were solid-fuel rockets powered by gunpowder . The inception of gunpowder rockets in warfare can be credited to the ancient Chinese, and in the 13th century, the Mongols played a pivotal role in ...
The Center for Simulation of Advanced Rockets (CSAR) is an interdisciplinary research group at the University of Illinois at Urbana-Champaign, and is part of the United States Department of Energy's Advanced Simulation and Computing Program. CSAR's goal is to accurately predict the performance, reliability, and safety of solid propellant ...
ILR-33 AMBER ([BURSZTYN] Error: {{Langx}}: invalid parameter: |ipa= ) is a Polish multistage suborbital rocket designed by Warsaw Institute of Aviation – Łukasiewicz Research Network. [3] The main goal of development of AMBER is gaining experience in building rocket engines and rockets themselves.
The rapid technological advances of the U.S. rocket industry during World War II, accomplished primarily through the wartime Office of Scientific Research and Development (OSRD) and its cadre of leading scientists, produced a substantial foundation of technical reports and data on solid rockets, propellants, and ballistics.
The Summerfield Research Station is a development and production site for solid rocket motors in the United Kingdom officially formed on 1 September 1951 by the Ministry of Supply. It was set up on the grounds of a former World War II munitions factory just south of Kidderminster, southwest of Birmingham.
For rocket-like propulsion systems, this is a function of mass fraction and exhaust velocity; mass fraction for rocket-like systems is usually limited by propulsion system weight and tankage weight. [ citation needed ] For a system to achieve this limit, the payload may need to be a negligible percentage of the vehicle, and so the practical ...
Solid rocket engine; thrusters; Hall-effect thruster; ammonia jet propulsion system; gas-jet propulsion system; used on Vega, Zenit, Cyclone and lot of soviet missiles; Okean-O, Sich-1, EgyptSat 1 and many Soviet spacecraft; Independence-X Aerospace: Malaysia ID-1, ID-2, ID-3 and unnamed 2-stage rocket engine for DNLV solid rocket motor and ...
NASA sounding rocket launch from the Wallops Flight Facility. The NASA Sounding Rocket Program (NSRP) is a NASA run program of sounding rockets which has been operating since 1959. [1] [2] The missions carried out by this program are primarily used for scientific research, particularly low gravity and material based research. [3]