ジャイロトロンを 用いた マイクロ波 ビーミング推進ロケットの開発
DESCRIPTION
若手科学者によるプラズマ研究会 2014/03/06. ジャイロトロンを 用いた マイクロ波 ビーミング推進ロケットの開発. 東京大学大学院 新領域創成科学研究科 先端エネルギー 工学専攻 福 成 雅史 山口敏和 小紫公也 共同研究： 日本原子力研究開発機構施設利用型共同研究・ 那珂核融合研究所 加熱工学グループ 宇宙航空研究開発機構・ 宇宙科学研究所 船木研究室. 目次. 超低コスト打ち上げ手段の必要性 ＝ マイクロ波ロケット開発の背景 ビーミング推進と超低コスト化のための三要素 研究開発の経過 エネルギー変換 の 物理：プラズマ・衝撃波の相互作用 - PowerPoint PPT PresentationTRANSCRIPT
Study of Interaction between Shock Wave and Plasma on Beamed Energy Propulsion and Technology around Microwave Propulsion
2014/03/06
kg10m30N2
kg
kg10m30N
ObjectiveMethodologyResults &DiscussionsConclusionsOverviewIntroductionkg#
SSPS1/50
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Space X, Falcon 9Scaled Composites, White Knight & Space Ship OnePD
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ObjectiveMethodologyResults &DiscussionsConclusionsOverviewIntroductionkg#
ObjectiveMethodologyResults &DiscussionsConclusionsOverviewIntroductionkg#1MWJAEA/
170 GHz< 1 MWGaussian40 mm50%
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ObjectiveMethodologyResults &DiscussionsConclusionsOverviewIntroductionkg#(PDE)Timep
p1xpp0(3)xpp0p1(2)xpp0(1)p0xpp < p0(4)ObjectiveMethodologyResults &DiscussionsConclusionsOverviewIntroductionkg#20032009
100, L300109 g Al
20092003600 kW, 100 Hz, 1.25 msec75 kW0.7 sec930 kW0.4 msecObjectiveMethodologyResults &DiscussionsConclusionsOverviewIntroductionkg#SSTOGEO100 km100 km10.2 km/s100 $/kg18GW
GEOKatsurayama et. al.H-IIBNNOIPPNNOIPPMicrowave RocketH-IIBObjectiveMethodologyResults &DiscussionsConclusionsOverviewIntroductionkg#
kg10m30N
OverviewMethodologyResults &DiscussionsIntroductionObjectiveConclusionskg#
pp1xOverviewMethodologyResults &DiscussionsIntroductionObjectiveConclusionskg#
: 610 kW
170GHz
OverviewMethodologyResults &DiscussionsIntroductionObjectiveConclusionskg#
30 kfps1 ms
30 kfps1 ms
OverviewMethodologyResults &DiscussionsIntroductionObjectiveConclusionskg#
180 mm from the second mirror(30 kfps, 1 ms)IR images (230-130 mm from the second mirror)
IR
Cm [N/MW]OverviewMethodologyResults &DiscussionsIntroductionObjectiveConclusionskg#
kg10m30N
OverviewResults &DiscussionsIntroductionObjectiveMethodologyConclusionskg#570kW,0.8ms200Hz530N
30N2011
30 Nat 570 kWwith 200 Hz520 mm56 mmKgOverviewResults &DiscussionsIntroductionObjectiveMethodologyConclusionskg# 182 m 120 mm40 mm10 kW/cm2100 kW/cm2f 60 mm 240 kW600 kW2m2m
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240 mm40 mm
OverviewResults &DiscussionsIntroductionObjectiveMethodologyConclusionskg# flowflowflowflowLow pressure High pressure Next pulse irradiationOverviewResults &DiscussionsIntroductionObjectiveMethodologyConclusionskg#kg21
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500 mmTimePropagation direction 555m/s0.4ms974m/sOverviewResults &DiscussionsIntroductionObjectiveMethodologyConclusionskg#
= 0.32
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Cmduty:
2.7N(Cm:28 N/MW)OverviewResults &DiscussionsIntroductionObjectiveMethodologyConclusionskg#
kg10mKg25kg (A), No. 23246145, , No. 253687.
Microwave RocketThe University of Tokyo26