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

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

Development of a combustion visualisation hybrid rocket motor

2017
The Phoenix Hybrid Sounding Rocket Programme in the University of KwaZulu-Natal's Mechanical Engineering department has so far only utilised pure paraffin wax and nitrous oxide as the propellant combination in their hybrid rockets. Knowledge of regression rate behaviour is required for the design and performance characterisation of hybrid rocket ...
Theba, R, Veale, KL, Bemont, CP
openaire   +1 more source

Performance of a unique hybrid rocket motor injector

32nd Joint Propulsion Conference and Exhibit, 1996
S. McCormick   +2 more
openaire   +1 more source

The opportunity for hybrid rocket motors in commercial space

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

Experimental Studies of Protrusion-Inserted Hybrid Rocket Motor with Varying L/D Ratio

Journal of Spacecraft and Rockets, 2021
Rajiv Kumar, Mengu Dinesh
exaly  

An evaluation of scaling effects for hybrid rocket motors

27th Joint Propulsion Conference, 1991
P. ESTEY, D. ALTMAN, J. MCFARLANE
openaire   +1 more source

Three-dimensional numerical simulation of hybrid rocket motor based on dynamic mesh technology

Aerospace Science and Technology, 2023
Guobiao Cai, Xiangyu Meng, Xiaoming Gu
exaly  

Vortex hybrid rocket motor

2023
CHIAVERINI MARTIN   +2 more
openaire   +2 more sources

Study of Regression Rates in a Hybrid Rocket Motor

AIAA Propulsion and Energy 2019 Forum, 2019
Jananee Dhanasekaran, Vikram Ramanan
openaire   +1 more source

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