Engines

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100k1

1000N type Thrust: 1000N-1200N Propellant: ethanol/LOX Duration: 20 seconds and over Others: abrative cooling, pressure-fed

DSC_0887a13
2000N type Thrust: 2000N-2500N Propellant: ethanol/LOX Duration: 100 seconds maximum Others: abrative cooling, pressure-fed
5000N type Thrust: 5000N Propellant: ethanol/LOX Duration: 100 seconds maximum Others: abrative cooling, pressure-fed
10kn
10 kN type Thrust: 10 kN Propellant: ethanol/LOX Duration: 100 seconds maximum Others: abrative cooling, pressure-fed enough total impulse for Sub-orbital flight above 100 km alt.

Commercial Flights

POCKY Mission Name: POCKY Launch Time: Nov. 11 2013, AM 11h11m11s Apogee: 1126m Length / Diameter / Weight: 3300mm / 118mm / 21.9kg Engine Thrust: 1000N Client: EZAKI GLICO CO.,LTD Others: First Commercial Rocket Launch in Japan The target of Apogee is 1111m

Demonstration Flights

SUZUKAZE Mission Name: SUZUKAZE (Cool wind) Launch Data: Aug. 8 2013 Apogee: 6553.6m Length / Diameter / Weight: 4322mm / 263mm / 113kg Engine Thrust: 5000N Others: Max speed is Mach 1.09 New downlink telemetry system
HINAMATSURI Mission Name: HINAMATSURI (Doll festival) Launch Data: Sep. 28 2012 Apogee: 0m Length / Diameter / Weight: 4173mm / 263mm / 98.5kg Engine Thrust: 2000N Others: Trouble of ground equipment system, It burn down a part of airframe
ICHIGO Mission Name: ICHIGO (Strawberry) Launch Data: Sep. 28 2012 Apogee: 1270m Length / Diameter / Weight: 4310mm / 262mm / 103kg Engine Thrust: 2000N Others: The plan of Apogee is 7000m Lost by strong wind Demonstrators
YUKIAKARI Mission Name: YUKIAKARI (Snow light) Launch Data: Dec. 17 2011 Apogee: 1001m Length / Diameter / Weight: 3768mm / 158mm / 29.65kg Engine Thrust: 1000N Others: New recovery system Land launch, Land recovery
NATSUMATSURI Mission Name: NATSUMATSURI (Summer festival) Launch Data: Jul. 23 2011 Apogee: 2000m Length / Diameter / Weight: 3920mm / 118mm / 24.7kg Engine Thrust: 1000N Others: Land launch, Sea recovery
HARUICHIBAN Mission Name: HARUICHIBAN (First spring storm) Launch Data: Mar. 26 2011 Apogee: 461m Length / Diameter / Weight: 3478mm / 118mm / 20.52kg Engine Thrust: 1000N Others First: launch Land launch, Land recovery

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