Simulations of Plain-Orifice Injection of Gelled Propellants Under Manifold Crossflow Conditions

2013 ◽  
Vol 29 (1) ◽  
pp. 136-146 ◽  
Author(s):  
Changjin Yoon ◽  
Stephen D. Heister ◽  
Charles L. Merkle ◽  
Guoping Xia
Keyword(s):  
Gelled Propellants

Characterization of impinging jet sprays of gelled propellants loaded with nanoparticles in the impact wave regime

Fuel ◽  
2018 ◽  
Vol 228 ◽  
pp. 10-22 ◽  
Author(s):  
Swarup Y. Jejurkar ◽  
Geetanjali Yadav ◽  
D.P. Mishra
Keyword(s):  
Impinging Jet ◽  
Wave Regime ◽  
Impact Wave ◽  
Gelled Propellants ◽  
The Impact

scholarly journals Green gelled propellant highly throtteable rocket motor and gas generator technology: status and application

2019 ◽  
Author(s):  
P. Caldas Pinto ◽  
H.K. Ciezki ◽  
K.W. Naumann ◽  
J. Ramsel ◽  
P. Kröger ◽  
...  
Keyword(s):  
Motor Development ◽  
Basic Research ◽  
Rocket Motor ◽  
Effective Control ◽  
Gas Generator ◽  
Component Level ◽  
Functional Aspects ◽  
Gelled Propellant ◽  
Ignition And Combustion ◽  
Gelled Propellants

Work on gel propulsion began in Germany in 1999. The German Gel Propulsion Technology (GGPT) Program started in 2001 from a white sheet of paper, proposed by the DLR Institute of Space Propulsion, Bayern-Chemie (BC), and the Fraunhofer Institute of Chemical Technology. Aim of the first phase was to develop the technology needed to build a rocket motor burning gelled propellants and to demonstrate its operability by a free flight within significantly less than a decade. The research and development activities were guided by a suitable principal concept for a gelled propellant rocket motor (GRM). Based on theoretical considerations (regarding functional aspects) and experimental pre-tests (propellant development, gelation, rheology, spraying, ignition, and combustion), a motor concept was pre-selected and the motor developed. The identified requirements were proven in December 2009 by two successful demonstration flights. The achieved know-how from basic research and technology (R+T) development has been consolidated in an application-oriented way on component level up to motor development. Within this scope, also, the goal of an effective control of the thrust by throttling the propellant mass flow rate (PMFR) while maintaining an optimum combustion chamber (CC) pressure could be achieved. This publication describes briefly several major advances in the development of the gel propulsion technology in Germany from rheology to combustor development to the thrust and pressure controller of a GRM.

Effects of Orifice Geometry on Gelled Propellants Sprayed from Impinging-Jet Injectors

2014 ◽  
Vol 30 (4) ◽  
pp. 1113-1117 ◽  
Author(s):  
Qing-fei Fu ◽  
Li-jun Yang ◽  
Kun-da Cui ◽  
Feng-chen Zhuang
Keyword(s):  
Impinging Jet ◽  
Gelled Propellants ◽  
Jet Injectors

Gelled propellants for tactical missile applications

1999 ◽  
Author(s):  
K. Hodge ◽  
T. Crofoot ◽  
S. Nelson
Keyword(s):  
Gelled Propellants
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