Abstract
The liquid rocket engine system design and analysis program has been developed for preliminary design process. The program performs system analysis according to input variables and requirements. It also seeks design variables with higher specific impulse and thrust-to-weight ratio via optimization technique such as genetic algorithm. Simple GUI was constructed for user convenience. Moreover, visualized design output can be figured in three-dimensional model via CATIA. The results are expected to be applied to analysis and selection of propulsion system, which is a part of preliminary design of launch vehicle.
| Original language | English |
|---|---|
| Title of host publication | 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference |
| Publisher | American Institute of Aeronautics and Astronautics Inc. |
| ISBN (Print) | 9781624102226 |
| DOIs | |
| State | Published - 2013 |
| Event | 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, JPC 2013 - San Jose, United States Duration: 14 Jul 2013 → 17 Jul 2013 |
Publication series
| Name | 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference |
|---|---|
| Volume | 1 PartF |
Conference
| Conference | 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, JPC 2013 |
|---|---|
| Country/Territory | United States |
| City | San Jose |
| Period | 14/07/13 → 17/07/13 |
Bibliographical note
Publisher Copyright:© 2013, American Institute of Aeronautics and Astronautics Inc. All rights reserved.