Results 201 to 210 of about 1,081 (242)

Laboratory-scale hybrid rocket motor uncertainty analysis

Journal of Propulsion and Power, 1996
Laboratory-scale hybrid rocket motors often provide the means to evaluate the burning rates of new fuel formulations. While the issue of scaling to larger sizes can be significant, the uncertainty level of the laboratory-scale results also needs evaluation.
R. A. Frederick, B. E. Greiner
openaire   +1 more source

Model of Hybrid Rocket Combustion in Classical Hybrid Rocket Motors

49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2013
Takakazu Morita, Saburo Yuasa, Toru Shimada, Shigeru Yamaguchi   +3 more
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, PASTRONE, Dario Giuseppe   +1 more
openaire   +2 more sources

Work In Progress: This is Rocket Science: Development and Testing of a Hybrid Rocket Motor in a Rocket Propulsion Course

Proceedings. Frontiers in Education. 36th Annual Conference, 2006
This paper describes a unique design and laboratory experience that was incorporated into an introductory rocket propulsion course. Specifically, each student team designed, built and tested a 7 lbf thrust hybrid rocket motor. The thrust chambers were fabricated from aluminum and the nozzles were fabricated from graphite.
openaire   +1 more source

Eco-Friendly Propellant for Hybrid Rocket Motor

2018
Conventional propulsion systems mostly based on the propellants which are highly toxic in nature. In a single rocket, the amount of such propellant is generally hundreds of tons. When this huge amount of propellant burnt, it develops a large amount of unburnt particles as well as gases which damage the ecosystem.
openaire   +1 more source

The DAEDUT/PMLTNO hybrid rocket motor facilities

1981
Aerospace ...
Schoyer, H.F.R. (author), Korting, P.A.O.G. (author)   +1 more
openaire   +1 more source

Development of a Hybrid Rocket Slab Motor

52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
Raisa Theba, Kirsty L. Veale, Clinton Bemont   +2 more
openaire   +1 more source

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

Numerical analysis of the hybrid rocket motor with axial injection based on oxidizer flow distribution

Acta Astronautica, 2022
Xianzhu Jiang, Ruipeng Yu, Yuanjun Zhang   +2 more
exaly  

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

Aerospace Science and Technology, 2021
Ruipeng Yu, Guobiao Cai, Yuanjun Zhang   +2 more
exaly