Characterization of Laser-Electric Hybrid Acceleration Plasma Thruster and System Development for Spacecraft Applications
Project/Area Number |
20360385
|
Research Category |
Grant-in-Aid for Scientific Research (B)
|
Allocation Type | Single-year Grants |
Section | 一般 |
Research Field |
Aerospace engineering
|
Research Institution | Tokai University |
Principal Investigator |
HORISAWA Hideyuki Tokai University, 工学部, 教授 (30256169)
|
Co-Investigator(Kenkyū-buntansha) |
FUNAKI Ikkoh 独立行政法人宇宙航空研究開発機構, 宇宙科学研究本部, 准教授 (50311171)
YAMAGUCHI Shigeru 東海大学, 理学部, 教授 (40297205)
|
Project Period (FY) |
2008 – 2010
|
Project Status |
Completed (Fiscal Year 2010)
|
Budget Amount *help |
¥19,500,000 (Direct Cost: ¥15,000,000、Indirect Cost: ¥4,500,000)
Fiscal Year 2010: ¥1,040,000 (Direct Cost: ¥800,000、Indirect Cost: ¥240,000)
Fiscal Year 2009: ¥1,040,000 (Direct Cost: ¥800,000、Indirect Cost: ¥240,000)
Fiscal Year 2008: ¥17,420,000 (Direct Cost: ¥13,400,000、Indirect Cost: ¥4,020,000)
|
Keywords | 推進 / エンジン / 宇宙推進機 / プラズマ推進機 / レーザ推進機 / レーザ電気複合推進機 / 航空宇宙工学 / ロケット / 人工衛星 / プラズマ・核融合 / 高性能レーザー |
Research Abstract |
A novel laser-electric hybrid acceleration system for space propulsion applications was developed and its feasibility study was conducted. From the thrust performance test, it was shown that high-specific-impulse operation up to 7,000 sec was achieved. In addition, developments of a compact high-power fiber laser system and a PID controlled thrust stand were conducted for onboard system components of micro spacecraft.
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Report
(4 results)
Research Products
(91 results)
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[Presentation] 微小推力測定装置の開発2010
Author(s)
與那嶺仁
Organizer
第54回宇宙科学技術連合講演会
Place of Presentation
静岡県コンベンションアーツセンター(静岡県)
Year and Date
2010-11-17
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