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http://dx.doi.org/10.5139/JKSAS.2003.31.3.072

Parametric Study on the Design of Hybrid Motor for Air Launch System  

Gwon, Sun Tak (건국대학교)
Lee, Chang Jin (건국대학교)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.31, no.3, 2003 , pp. 72-78 More about this Journal
Abstract
In this paper, the feasibility study and the parametric design of hybrid motor with HTPB/LOX were conducted for micro air launch system. Design results were compared with 1st stage of Pegasus XL for verification of hybrid motor. Results showed that hybrid motor replace solid booster if Isp of hybrid motor reaches 330sec. In addition, mission analysis was established for micro air launch system, and parametric design was conducted with design variables: number of port, initial oxidizer flux, and chamber pressure. And the region of Isp was identified by parametric study which satisfied design constraints and mission analysis.
Keywords
Air Launch System; Hybrid Motor; HTPB/LOX; Preliminary Design;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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