Experimental Study of a Laser-Ignited Liquid Cryogenic Rocket Engine

2015 ◽  
Author(s):  
Michael Börner ◽  
Chiara Manfletti ◽  
Alex Grebe ◽  
Stefan Gröning ◽  
Justin Hardi ◽  
...  
Keyword(s):  
Experimental Study ◽  
Rocket Engine

Experimental Study and Simulation of Rocket Engine Freejet Noise

AIAA Journal ◽  
2001 ◽  
Vol 39 (10) ◽  
pp. 1851-1859 ◽  
Author(s):  
Jean Varnier
Keyword(s):  
Experimental Study ◽  
Rocket Engine

Experimental study of lunar-based hybrid rocket engine

2021 ◽  
Author(s):  
Umit Yelken ◽  
Ali Yalcintas ◽  
Ozan Kara ◽  
Mustafa Baysal ◽  
M. Arif Karabeyoglu
Keyword(s):  
Experimental Study ◽  
Rocket Engine ◽  
Hybrid Rocket ◽  
Hybrid Rocket Engine

Experimental Study on the Possibilities to Decrease the Coefficient of Restitution after Impact

2012 ◽  
Vol 217-219 ◽  
pp. 1659-1662 ◽  
Author(s):  
Todor Nikolov Penchev ◽  
Ivan Lyubomirov Altaparmakov ◽  
Dimitar Nedelchev Karastojanov
Keyword(s):  
Experimental Study ◽  
Laboratory Test ◽  
Experimental Research ◽  
Rocket Engine ◽  
Coefficient Of Restitution ◽  
Compressed Air ◽  
Pile Driving ◽  
Additional Force ◽  
Forging Die ◽  
Two Bodies

Technological processes such as forging, die forging, pile driving, etc., are realized as a result of a collision between two bodies. The bodies’ rebound after the collision takes place due to the use of part of the energy of the hit for their elastic deformation. The paper presents results from an experimental research on the possibilities of the decrease of rebound, by the use of an additional force during the hit. A laboratory test-stand is described in which an additional force is created by the use of a cold rocket engine, working with compressed air.

Experimental study on combustion characteristics of powder magnesium and carbon dioxide in rocket engine

2019 ◽  
Vol 155 ◽  
pp. 334-349 ◽  
Author(s):  
Yue Li ◽  
Chunbo Hu ◽  
Xiaofei Zhu ◽  
Jiaming Hu ◽  
Xu Hu ◽  
...  
Keyword(s):  
Carbon Dioxide ◽  
Experimental Study ◽  
Rocket Engine ◽  
Combustion Characteristics

Experimental Study of Ejectors’ Effect on the Performance of Pulse Detonation Rocket Engine

2014 ◽  
Vol 628 ◽  
pp. 293-298 ◽  
Author(s):  
Qiao Dong Bai ◽  
Chun Sheng Weng
Keyword(s):  
Experimental Study ◽  
Relative Position ◽  
Rocket Engine ◽  
Experimental Studies ◽  
Experimental Results ◽  
Operating Frequency ◽  
Pulse Detonation ◽  
Pulse Detonation Rocket Engine ◽  
Maximum Thrust

Experimental studies were performed to investigate the ejector’s effect on the performance of a pulse detonation rocket engine (PDRE). The PDRE employed in the experiments utilizes gasoline as fuel and air as oxidizer. The operating frequency of the PDRE is 10 and 20 Hz respectively. Performance is quantified by thrust measurements, and the average thrust of the PDRE is obtained by integration of the thrust measured in the experiment. The experimental results show that the PDRE can increase thrust augmentation with an ejector, a maximum thrust augmentation is measured by 18.7% at 10 Hz operating frequency. In the experiment, axial placement (X/DPDRE) of the ejector is varied downstream the PDRE tube of 0.5,1 and 2 respectively. It is found that the thrust augmentation obviously increases when the relative position at 1 and 2, and also the thrust augmentation increases at higher operating frequency. The experiment result is useful for the development of a PDRE producing higher thrust.

Sign in / Sign up

Export Citation Format

Share Document