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Integrated Design-Trajectory Optimization for Hybrid Rocket Motors

2012
Hybrid rocket motors present a competitive edge among space applications, as they are flexible, safe, reliable, and low cost. The motor design and operation are contingent on the type of designated mission; therefore, it is useful to couple design and trajectory optimization.
PASTRONE, Dario Giuseppe   +1 more
openaire   +2 more sources

Model of Hybrid Rocket Combustion in Classical Hybrid Rocket Motors

49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2013
Takakazu Morita   +3 more
openaire   +1 more source

Performance Prediction Software for Hybrid Rocket Motors

Procceedings of the 18th Brazilian Congress of Thermal Sciences and Engineering, 2020
Renato Filho, Maurício Sá Gontijo
openaire   +1 more source

Hybrid rocket motor propellant selection alternatives

28th Joint Propulsion Conference and Exhibit, 1992
PAUL ESTEY, GEORGE WHITTINGHILL
openaire   +1 more source

A Parametric Analysis of Hybrid Rocket Motors for Sounding Rockets

44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2008
CASALINO, LORENZO   +1 more
openaire   +2 more sources

Development of a Hybrid Rocket Slab Motor

52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
Raisa Theba   +2 more
openaire   +1 more source

Restartable Hybrid Rocket Motor using Nitrous Oxide

57th International Astronautical Congress, 2006
Vadim Zakirov   +4 more
openaire   +1 more source

Transient investigation of nozzle erosion in a long-time working hybrid rocket motor

Aerospace Science and Technology, 2021
Guobiao Cai, Yuanjun Zhang
exaly  

Experimental and numerical study on slag deposition in solid rocket motor

Aerospace Science and Technology, 2022
Baolu Shi
exaly  

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