Results 101 to 110 of about 1,005,662 (212)
Combustion characterization of ammonium perchlorate based solid rocket propellant [PDF]
, 2011 There were many studies on ammonium perchlorate (AP) based solid rocket propellant (SRP) and some data already exist. However, there is no complete data available in Malaysia especially the information on the combustion characteristics of baseline data ...
Aziz, Amir
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Advanced Technology Upper Stages for Future Launchers [PDF]
, 2010 The paper describes two different preliminary system designs for stages employing advanced technologies: 1. An experimental micro-stage with a very small storable propellant engine for LEO applications. This vehicle is part of the multinational (France,
Gerstmann, Jens +4 more
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Performance of composite solid rocket propellants for rocket assisted projectiles (RAP) [PDF]
The International Conference on Chemical and Environmental Engineering, 2016 Mohamed Nawwar +2 more
openaire +1 more source
, 2010 Control over drop size distributions, injection rates, and geometrical distribution of fuel and oxidizer sprays in bi-propellant rocket engines has the potential to produce more efficient, more stable, less polluting rocket engines.
Coletti, M. +4 more
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Development of solid rocket propellant [PDF]
, 2012 This thesis presents a study on development of solid rocket propellant that was carried out at Universiti Malaysia Pahang. Rocket propellant has been identified as a component that played an important role in the development of rockets.
Mohammad Norshim, Mohamed Hashim
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Anomalous Behavior of a Solid Rocket Motor Nozzle Insert During Static Firing Test
Journal of Aerospace Technology and Management, 2016 This paper presents the study and development of a firing test used to evaluate the behavior of a solid rocket motor. The motivation for the development of a subscale solid rocket motor with end burning propellant grain geometry arose from the need to ...
Ronald Izidoro Reis +2 more
doaj
A Reliable Method for Predicting the Specific Impulse of Chemical Propellants
Journal of Aerospace Technology and Management, 2018 The specific impulse (Isp) is an important performance parameter that describes energy efficiency of propellant combustion and is intimately related to the rocket engine thrust.
Dany Frem
doaj
Future European Expendable Launcher Options and Technology Preparation [PDF]
, 2008 The paper describes latest results of the most recent activities in Germany in the technical assessment of future European launcher architecture. In a joint effort of DLR-SART with German launcher industry a next generation upper-medium class expendable ...
Gerstmann, Jens +6 more
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Improving the Mechanical Properties of Composite Rocket Propellants
, 2004 Solid composite rocket propellants usually contain ammoniumperchlorate embedded in an elastic polymer binder. The bindercan be based on a liquid prepolymer such as hydroxyl-terminatedpolybutadiene, HTPB, or poly(3-nitratomethyl-3-methyl oxetane,PolyNIMMO.
openaire +1 more source
Studies on Modification of Formulations of Composite Solid Propellant for Dual Thrust Rocket Motor [PDF]
, 2011 W pracy przedstawiono wyniki z badań zmodyfikowanych ładunków napędowych dla dwuzakresowego silnika rakietowego. Modyfikacja polegała na optymalizacji składu heterogenicznego paliwa rakietowego na bazie nadchloranu amonu jako utleniacza i lepiszcza na ...
Florczak, B., Cholewiak, A.
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