DC Field | Value | Language |
---|---|---|
dc.contributor.author | Moon, Yongjun | ko |
dc.contributor.author | Jang, Tae Seong | ko |
dc.contributor.author | Park, Chul | ko |
dc.contributor.author | Kwon, Sejin | ko |
dc.date.accessioned | 2013-08-14T01:10:25Z | - |
dc.date.available | 2013-08-14T01:10:25Z | - |
dc.date.created | 2013-08-09 | - |
dc.date.created | 2013-08-09 | - |
dc.date.issued | 2013-05 | - |
dc.identifier.citation | JOURNAL OF SPACECRAFT AND ROCKETS, v.50, no.3, pp.620 - 631 | - |
dc.identifier.issn | 0022-4650 | - |
dc.identifier.uri | http://hdl.handle.net/10203/175050 | - |
dc.description.abstract | Requirements of a propulsion system for lunar-exploration missions using a launch vehicle, the development of which has recently started in Korea, were conceptualized. A new three-stage-to-orbit launch system, the Korea Space Launch Vehicle 2 will be a middle-class launch vehicle in that its expected payload capacity to low Earth orbit will be about 2.6 tons. The Korea Space Launch Vehicle 2 is under development and may possibly launch a lunar orbiter and a lander within 10-15 years. Considering some of the limitations and requirements a new space-propulsion system must be developed, and it has been found that a H2O2/kerosene-bipropellant rocket is the optimum propulsion system among several types of chemical rockets. The optimum thrust and burn-time requirements for orbital transfers and landing using H2O2/kerosene-bipropellant rockets were also derived by mass budget design and three-degree-of-freedom orbit-trajectory calculations. It has been found that, using the Korea Space Launch Vehicle 2,1800 N-class H2O2/kerosene-bipropellant propulsion system with a continuous burn time of more than 340s and an accumulated burn time of more than 710 s needs to be developed for the lunar-exploration missions. | - |
dc.language | English | - |
dc.publisher | AMER INST AERONAUTICS ASTRONAUTICS | - |
dc.title | Requirements Analysis of Propulsion Systems for Lunar-Exploration Mission | - |
dc.type | Article | - |
dc.identifier.wosid | 000320091200013 | - |
dc.identifier.scopusid | 2-s2.0-84878775311 | - |
dc.type.rims | ART | - |
dc.citation.volume | 50 | - |
dc.citation.issue | 3 | - |
dc.citation.beginningpage | 620 | - |
dc.citation.endingpage | 631 | - |
dc.citation.publicationname | JOURNAL OF SPACECRAFT AND ROCKETS | - |
dc.identifier.doi | 10.2514/1.A32349 | - |
dc.embargo.liftdate | 9999-12-31 | - |
dc.embargo.terms | 9999-12-31 | - |
dc.contributor.localauthor | Jang, Tae Seong | - |
dc.contributor.localauthor | Kwon, Sejin | - |
dc.contributor.nonIdAuthor | Moon, Yongjun | - |
dc.type.journalArticle | Article; Proceedings Paper | - |
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