Design specifications of H2O2/kerosene bipropellant rocket system for space missions
- Author
- YONGJUN MOON1 ; CHUL PARK1 ; SUNGKWON JO2 ; SEJIN KWON1
[1] Korea Advanced Institute of Science and Technology, Daejeon 305-701, Korea, Republic of
[2] Korea Institute of Machinery and Materials, Daejeon 305-343, Korea, Republic of - Source
Aerospace science and technology (Imprimé). 2014, Vol 33, pp 118-121, 4 p ; ref : 29 ref
- ISSN
- 1270-9638
- Scientific domain
- Aeronautics astronautics; Mechanics acoustics
- Publisher
- Elsevier, Issy-les-Moulineaux
- Publication country
- France
- Document type
- Article
- Language
- English
- Author keyword
- Apogee kick motor Design optimization H2O2/kerosene bipropellant rocket system Propulsion specifications
- Keyword (fr)
- Conception optimale Fluide propulseur Hydrocarbure Kérosène Peroxyde d'hydrogène Satellite artificiel Satellite géostationnaire Système propulsion
- Keyword (en)
- Optimal design Propellant fluid Hydrocarbons Kerosene Hydrogen peroxide Artificial satellites Geostationary satellite Propulsion systems
- Keyword (es)
- Concepción optimal Fluido propulsor Peróxido de hydrogeno Satélite geoestacionario
- Classification
- Pascal
- 001 Exact sciences and technology / 001E Earth, ocean, space / 001E03 Astronomy / 001E03A Fundamental astronomy and astrophysics. Instrumentation, techniques, and astronomical observations / 001E03A40 Artificial earth satellites
- Discipline
- Astronomy
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 28331784
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
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DOI
10.1016/j.ast.2014.01.006 
https://dx.doi.org/10.1016/j.ast.2014.01.006
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