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Rocket propulsion
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131	Technical papers Hybrid safety While there is no doubt that hybrids are considerably safer than traditional solid or liquid rocket engines, there is a popular misconception that they are totally safe, and never go boom. Add to Reading List Source URL: myweb.tiscali.co.uk Language: English - Date: 2010-01-19 09:42:27 Rocket propulsion Spacecraft propulsion Rocketry Dissociative drugs Rocket propellants Nitrous oxide engine Hybrid rocket Nitrous oxide Liquid-propellant rocket Transport Space technology Technology
132	Technical papers Introduction to hybrid design The following is a short introduction to hybrid rocket engines, with some examples of the current state of hybrid research around the world. Words in bold appear in the Glo Add to Reading List Source URL: myweb.tiscali.co.uk Language: English - Date: 2010-01-19 09:42:44 Aerospace engineering Rocket propulsion Rocket engines Rocketry Pyrotechnics Hybrid rocket Liquid-propellant rocket Solid-fuel rocket Internal combustion engine Space technology Spacecraft propulsion Transport
133	Technical papers The physics of Nitrous Oxide Introduction Most amateur rocketry groups choose Nitrous oxide, often referred to as ‘nitrous’, and sometimes ‘nitrogenous oxide’ or ‘dinitrogen oxide’, (though Add to Reading List Source URL: myweb.tiscali.co.uk Language: English - Date: 2011-07-16 15:03:00 Gases Chemical properties Spacecraft propulsion Phase transitions Nitrous oxide engine Nitrous oxide Hybrid rocket Triple point Supercritical fluid Chemistry Physics Thermodynamics
134	Government to invest £60 million in world’s first airbreathing rocket engine Through the UK Space Agency, the Government is set to invest £60 million in the development of the SABRE - a British-designed rocket engine Add to Reading List Source URL: www.reactionengines.co.uk Language: English - Date: 2015-02-03 11:49:38 British space programme Emerging technologies Spacecraft propulsion Single-stage-to-orbit Spaceplanes Skylon Reaction Engines Limited SABRE Space Shuttle Aerospace engineering Space technology Spaceflight
135	Journal of Polymer and Biopolymer Physics Chemistry, 2014, Vol. 2, No. 4, 78-83 Available online at http://pubs.sciepub.com/jpbpc/2/4/4 © Science and Education Publishing DOI:[removed]jpbpc[removed]Review on the Fundamen Add to Reading List Source URL: www.sciepub.com Language: English Spacecraft propulsion Polymer chemistry Synthetic fibers Rocket engines Polymer Combustion Hybrid rocket Aramid Calorimeter Chemistry Materials science Organic polymers
136	Technical series A Dynamic stability analysis rocket simulator Introduction: The basic static stability of the fixed-fin rocket vehicles that we fly has been covered by Barrowman’s superb analysis (Ref’s 4, 5), and Add to Reading List Source URL: myweb.tiscali.co.uk Language: English - Date: 2011-06-11 15:22:53 Aerospace engineering Rocket propulsion Mechanics Rotation Jet damping Moment of inertia Flight dynamics Rocket Stability derivatives Physics Space technology Aerodynamics
137	Plasma Adiabaticity in a Diverging Magnetic Nozzle IEPC[removed]Presented at the 33rd International Electric Propulsion Conference, The George Washington University, Washington, D.C., USA October 6–10, 2013 J. P. Shee Add to Reading List Source URL: www.umich.edu Language: English - Date: 2013-10-22 10:51:46 Optical materials Plasma Double layer Langmuir probe Variable Specific Impulse Magnetoplasma Rocket Helicon Electron Helicon Double Layer Thruster Ion thruster Plasma physics Physics Spacecraft propulsion
138	Technical papers Modelling the nitrous run tank emptying Introduction This paper describes mathematical models of the emptying of a tank of saturated nitrous oxide that empties purely due to its self pressure. This is s Add to Reading List Source URL: myweb.tiscali.co.uk Language: English - Date: 2011-07-16 15:02:45 Spacecraft propulsion Nitrous oxide engine Rocket propulsion Nitrous oxide Hybrid rocket Combustion Rocket engine Heat capacity Transport Chemistry Space technology
139	Technical papers Hybrid effects on vehicle stability Ammendment Earlier editions of this paper contained a formula from reference 1 for calculating the moment of inertia of a liquid propellant in a cylindrical tank. Thi Add to Reading List Source URL: myweb.tiscali.co.uk Language: English - Date: 2010-11-08 14:50:06 Rocketry Pyrotechnics Spacecraft propulsion Slosh dynamics Rocket Propellant Moment of inertia Nitrous oxide engine Nitrous oxide Physics Space technology Transport
140	JOURNAL OF PROPULSION AND POWER Vol. 27, No. 4, July–August 2011 Technical Notes Downloaded by UNIVERSITY OF MICHIGAN on February 28, 2013 \| http://arc.aiaa.org \| DOI: [removed] Add to Reading List Source URL: www.umich.edu Language: English - Date: 2013-02-28 10:36:28 Physics Variable Specific Impulse Magnetoplasma Rocket Ion thruster Plasma propulsion engine Helicon Double Layer Thruster Plasma Hall effect thruster Helicon Specific impulse Spacecraft propulsion Aerospace engineering Propulsion

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