Engines

usually not for sale

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

Video