Download - 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
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
http://www.rish.kyoto-u.ac.jp/space/people/shino/research-sps2.htmJAXAH2BM-VPPTObjectiveMethodologyResults &DiscussionsConclusionsOverviewIntroductionkg#
Space X, Falcon 9Scaled Composites, White Knight & Space Ship OnePD
ISAS/JAXA
PD
Scaled CompositesWhite KnightSpace Ship One
ObjectiveMethodologyResults &DiscussionsConclusionsOverviewIntroductionkg#
ObjectiveMethodologyResults &DiscussionsConclusionsOverviewIntroductionkg#1MWJAEA/
170 GHz< 1 MWGaussian40 mm50%
ITERMW 0.1 msec - 1,000 sec5 kHzJAEA : 3 m / : 800 kg
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
OverviewResults &DiscussionsIntroductionObjectiveMethodologyConclusionskg#
240 mm40 mm
OverviewResults &DiscussionsIntroductionObjectiveMethodologyConclusionskg# flowflowflowflowLow pressure High pressure Next pulse irradiationOverviewResults &DiscussionsIntroductionObjectiveMethodologyConclusionskg#kg21
()Osc.OverviewResults &DiscussionsIntroductionObjectiveMethodologyConclusionskg#
500 mmTimePropagation direction 555m/s0.4ms974m/sOverviewResults &DiscussionsIntroductionObjectiveMethodologyConclusionskg#
= 0.32
OverviewResults &DiscussionsIntroductionObjectiveMethodologyConclusionskg#duty = 0.2duty = 0.1duty = 0.05duty = 0.02duty = 0.01duty = 0.5Kgduty0.2
Cmduty:
2.7N(Cm:28 N/MW)OverviewResults &DiscussionsIntroductionObjectiveMethodologyConclusionskg#
kg10mKg25kg (A), No. 23246145, , No. 253687.
Microwave RocketThe University of Tokyo26