The week's pick
Random Articles
Reseach Article
Multidisciplinary Design Optimization of Hydrogen Peroxide Monopropellant Propulsion System using GA and SQP
| International Journal of Computer Applications |
| Foundation of Computer Science (FCS), NY, USA |
| Volume 113 - Number 9 |
| Year of Publication: 2015 |
| Authors: Amirhossein Adami, Mahdi Mortazavi, Mehran Nosratollahi |
10.5120/19853-1774
|
Amirhossein Adami, Mahdi Mortazavi, Mehran Nosratollahi . Multidisciplinary Design Optimization of Hydrogen Peroxide Monopropellant Propulsion System using GA and SQP. International Journal of Computer Applications. 113, 9 ( March 2015), 14-21. DOI=10.5120/19853-1774
Abstract
An intense simplification in production, storage and handling of hydrogen peroxide develop a renewed interest in hydrogen peroxide thrusters especially for low cost attitude control or orbit correction (orbit maintenance). Chemical decomposition, aerothermodynamics flow and structure demand different optimum conditions such as tank pressure, catalyst bed pressure, concentration of H2O2 and geometry. These parameters play important role in propulsion system's mass and performance. Discipline conflicts are solved by Multidisciplinary Design Optimization (MDO) techniques with synchronized optimization for all subsystems respect to any criteria and limitations. In this paper, monopropellant propulsion system design optimization algorithm is presented and result of the design algorithm is validated. Results of the design algorithm have been compared with data of two different operational thrusters. According to the results, the proposed model can suitably predict total mass and performance with errors below than 10%. Then, MDO framework is proposed for the monopropellant propulsion system. Optimum propellant mass, thrust level, mass flow rate, nozzle geometry, catalyst bed length and diameter, propellant tank mass, feeding subsystem mass and total mass are derived using hybrid optimization (GA+SQP) for two space missions.
References
- Design specifications of H2O2/kerosene bipropellant rocket system for space missions. Yongjun Moona, Chul Park,Sungkwon Jo,Sejin Kwon. Issue1,Pages 118–121, Aerospace Science and Technology, February 2014, Vol. 33.
- An Application of Commercial Grade Hydrogen Peroxide for Hybrid/Liquid Rocket Engine. Tsujikado, N. , Koshimae, M. , Ishikawa, R. , Kitahara, K. , Ishihara, A. , Sakai, Y. , and. Indianapolis, Indiana : 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 7-10 July , 2002. AIAA paper 2002-3573.
- Deign and Testing of an Upper Stage Hybrid Propulsion System Using Hydrogen Peroxide Oxidizer. A. S. Prince, R. L. Carpenter, T. A. Boardman. Huntsville, Alabama : 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2002.
- Validation and Design Optimization for a Hydrogen Peroxide Thruster. R-J. Koopmans, J. S. Shrimpton and G. T. Roberts. San Diego, California : 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 31 July - 03 August 2011, 2011. AIAA 2011-5696.
- Monopropellant Hydrogen Peroxide Rocket Systems Optimum for Small Scale. Wernimont, E. J. Sacramento,CA. : 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference& Exhibit, 2006. AIAA-2006-5235.
- A Monopropellant Milli-Newton Thruster System for Attitude Control of Nanosatellites. Platt, Donald. 16th Annual USU Conference on Small Satellites, 2002. SSC02-VII-4.
- Catalyst Bed Testing for Development of a 98% Hydrogen Peroxide Procurement Specification. Wernimont, E. and Ventura, M. 2002. AIAA paper 2002-3852.
- Hydrogen Peroxide Decomposition on Various Supported Catalysts Effect of Stabilizers. Pirault-Roy, L. , Kappenstein, C. , Guerin, M. , Eloirdi, R. , and Pillet, N. ,. No. 6, pp. 1235–1241, Journal of Propulsion and Power, 2002, Vol. 18.
- Decomposition of Hydrogen Peroxide on MnO2/TiO2 Catalysts. Sorge, A. R. , Turco, M. , Pilme, G. , Bagnasco, G. No. 6, pp. 1069-1075, Journal of Propulsion and Power, Nov. -Dec, Vol. 20.
- Hydrogen Peroxide Thruster Module for Microsatellites with Platinum Supported by Alumina as Catalyst. An, S. , Lim, H. , and Kwon, S. Cincinnati, OH , 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 8-11,2007. AIAA-2007-5467.
- Experimental Characterization of a 5 N Hydrogen Peroxide. A. Pasini, L. Torre and et al. American Institute of Aeronautics and Astronautics.
- Assessment of High Performance HAN Monopropellants. Wucherer E. J. , Christofferson S. and Reed B. Huntsville, Alabama : AIAA, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. No. 2000-3872.
- An Overview of the Development of HNF and HNF-based Propellants. H. F. R. Schoyer, P. A. O. G. Korting , W. H. M. Veltmans , Louwers J. , A. E. D. M Heijden, H. L. J. Keizers and V. D. Berg. Huntsville, Alabama : 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. No. 2000-3184.
- Multidisciplinary design optimization of a reentry vehicle using genetic algorithm. M. Nosratollahi, M. Mortazavi, A. Adami, M. Hosseini. 3, pp. 194-203, Aircraft Engineerirng and Aerospace Technology, 2010, Vol. 82.
- DESIGN AND TESTING OF A 50N HYDROGEN PEROXIDE MONOPROPELLANT ROCKET THRUSTER. Norazila Othman, Subramaniam Krishnan, Wan Khairuddin and et al. Jurnal Mekanikal, December 2011, Vols. No 33, 70-81.
- Amirhossein Adami. Multidicsiplinary design optimization of Reentry Vehicle considering Guidance Algorithm. Tehran, Iran : Amirkabir University Of technology,, 2014. P. hd thesis.
- Development of a HTP Mono-propellant Thruster by Using Composite Silver Catalys. Y. A. Chan, H. W. Hsu, and Y. C. Chao. San Deigo, CA : 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 31 July - 3 August, 2011.
- Preliminary Development of a Hydrogen Peroxide Thruster. Y. A. Chan, H. J. Liu, K. C. Tseng, and T. C. Kuo. World Academy of Science, Engineering and Technology, 2013-07-21, Vol. 79. pp:1226-1233.
Index Terms
Keywords