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Design and development of hybrid rocket [PDF]

The goal of University of Queensland's hybrid rocket team for 2005 was to study the regression behavior of Perspex (PMMA) and Poly Vinyl Chloride (PVC) in order to optimize the performance of the hybrid rocket and eventually lead to a flight version. In 2005, the team successfully conducted 13 hybrid rocket firings, gathering data for 11 of these tests.
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Hybrid rocket development at the American Rocket Company

26th Joint Propulsion Conference, 1990
R. KNIFFEN, BEVIN MCKINNEY, PAUL ESTEY
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Design and development of a hybrid rocket

A hybrid rocket is a propulsion system that uses a combination of solid fuel and liquid or gaseous oxidiser (Sutton 1992). Hybrids have many advantages, including their relative safety, minimal impact on the environment, low cost as compared to other forms of rockets, and their ability to be throttled.
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Hybrid Rocket Theory and Design

1968
A hybrid rocket is so named because one of the propellant components is liquid and the other solid. Normally the oxidizer is liquid and the fuel is solid. In a typical design (Fig. 7-1), the oxidizer is sprayed in at the head end of a solid cylindrical fuel grain. It is apparent that once the liquid oxidizer is injected, the combustion process proceeds
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Utilization of additive manufacturing in hybrid rocket technology: A review

Acta Astronautica, 2021
Çagri Oztan
exaly  

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
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Demonstration of tethered hovering flight of HTTP-3AT hybrid rocket

Acta Astronautica, 2022
Ming-Tzu Ho, Sho-Tsung Kao, Yang Lee
exaly  

Large-Scale CAMUI Type Hybrid Rocket Motor Scaling, Modeling, and Test Results

Aerospace, 2022
Harunori Nagata, Landon Kamps, Kazuo Yonekura   +2 more
exaly  

Transient combustion in hybrid rockets

31st Joint Propulsion Conference and Exhibit, 1995
M Karabeyoglu, D Altman, D Bershader
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On use of hybrid rocket propulsion for suborbital vehicles

Acta Astronautica, 2018
Adam Okniński
exaly