Nanoparticles for solid rocket propulsion

2006 ◽  
Vol 18 (33) ◽  
pp. S1991-S2005 ◽  
Author(s):  
L Galfetti ◽  
L T De Luca ◽  
F Severini ◽  
L Meda ◽  
G Marra ◽  
...  
Keyword(s):  
Rocket Propulsion ◽  
Solid Rocket

INNOVATIVE METAL FUELS FOR SOLID ROCKET PROPULSION

2012 ◽  
Vol 11 (4) ◽  
pp. 299-322 ◽  
Author(s):  
Stefano Dossi ◽  
Alice Reina ◽  
Filippo Maggi ◽  
L. T. De Luca
Keyword(s):  
Rocket Propulsion ◽  
Solid Rocket

Design Optimization of Solid Rocket Propulsion: A Survey of Recent Advancements

2020 ◽  
Vol 57 (1) ◽  
pp. 3-11
Author(s):  
Ahmed Mahjub ◽  
Nurul Musfirah Mazlan ◽  
M. Z. Abdullah ◽  
Qummare Azam
Keyword(s):  
Design Optimization ◽  
Rocket Propulsion ◽  
Solid Rocket

Design of a Solid Rocket Motor for Characterization of Spinning

2011 ◽  
Vol 63-64 ◽  
pp. 621-626
Author(s):  
Zai Cheng Wang ◽  
Chun Lan Jiang ◽  
Ming Li
Keyword(s):  
Rocket Motor ◽  
Structure Characterization ◽  
Test Results ◽  
Solid Rocket Motor ◽  
Ballistic Performance ◽  
Static Test ◽  
Rocket Propulsion ◽  
Working Performance ◽  
Solid Rocket

Although the rocket propulsion technologies have been used for several decades, the traditional motor can not meet the special rotating requirement. A kind of spinning solid rocket motor (SSRM) which used as power device of some kinds of dispenser was introduced. This kind of motor has the structure characterization for tangential nozzles. Its design scheme and prediction of interior ballistic performance were discussed. And the main factors should to be considered in design were analyzed comprehensively. In order to research working performance of the SSRM static test was carried out. The calculation and test results indicate that the design can satisfy general requirement of its application normally.

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