Special Issue : Recent Progress in Research and Development of Hybrid Rocket / PART 2 . - Research activities of University and Amateurs - [PDF]
, 2002 Min-Chan Gwon, Hwan-Il Heo
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Design and Optimization of a Hybrid Gas Generator for Hydrogen Peroxide Tank Pressurization
Challenges and Issues of Modern SciencePurpose. This study develops a pressurization system for hydrogen peroxide tanks using a hybrid gas generator powered by liquid oxygen and solid fuel.
Mykhailo Vorobei, Mykola Bondarenko
doaj
Journal of Aerospace Technology and Management, 2013 http://dx.doi.org/10.5028/jatm.v5i3.228 Experimental investigation was conducted to determine the relative propulsive and combustion behavior of several polyurethane-based solid-fuel formulations containing 30% w/w of paraffin or 10% of aluminum powder.
Susane Ribeiro Gomes +3 more
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Numerical modelling of the hybrid rocket engine performance
Propulsion and Power Research, 2021 The purpose of this paper is to present method of the numerical modeling of the hybrid rocket engine's work as a tool for designing engines of this type.
Marian Gieras, Aleksander Gorgeri
doaj
Mars Ascent Vehicle - Payload?, Spacecraft?, Launch Vehicle? - A Systems Approach to MAV [PDF]
Significant effort has been expended over the past few years in order to examine propulsion technologies for an eventual robotic Mars Ascent Vehicle (MAV).
Bishop, Karen +3 more
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Design of a Hybrid Lunar-fueled Rocket
, 2021 Today, our calling to explore the universe is even greater than fifty years ago, this calls out for a new design in our propulsion systems in order to achieve a sustainable, reusable and Earth-conditions independent. Sixty years ago, the worldwide known as the space race started. The first step on the Moon by a Homo Sapiens Sapiens was the end point on
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Design issues for lunar in situ aluminum/oxygen propellant rocket engines [PDF]
Design issues for lunar ascent and lunar descent rocket engines fueled by aluminum/oxygen propellant produced in situ at the lunar surface were evaluated.
Meyer, Michael L.
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Diversity of Safety Arguments in the Validation of a Sounding Rocket Destruction System [PDF]
, 2001 This work describes an approach for the validation of a software system responsible for the destruction of the sounding rocket VS-40X. The process of validation uses three different techniques ranging from the automatic state exploration to the laborious
Abdala, M.A.D. +2 more
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Lower hybrid waves observed at the dayside polar region: SS‐520‐2 rocket experiment [PDF]
, 2003 Yoshikatsu Ueda +6 more
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Hybrid propulsion technology program. Volume 1: Conceptional design package [PDF]
A concept design study was performed to configure two sizes of hybrid boosters; one which duplicates the advanced shuttle rocket motor vacuum thrust time curve and a smaller, quarter thrust level booster.
Holzman, Allen L. +5 more
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