Rocket Engine: HyperTEK HT440-076-J115
Oxidizer: Nitrous Oxide
Fuel: plastic
Mass of the Empty Oxidizer Tank: 494,4 g
Mass of the Injector: 161,4 g
Mass of the Fuel Tube when new: 382,3 g
Mass of the Fuel Tube when used: 352,8 g
Ignition: High-Voltage Spark and Oxygen
Flight Computer: MAWD miniAlt/WD logging dual event altimeter
Rocket frame: HyperLOC 835
Height of the Launch Platform: 2,5 m
Distance of the Launch Control from the Launch Platform: 30 m
Rocket Launch Mass: 3,4 kg
Rocket Max Altitude: 1,1 km
Time of Rocket Max Altitude: 15,65 s
Burn Time of the Engine: 6,7 s
Rocket Max Velocity: 130 m/s
Rocket Max Acceleration: 6,8 g
Engine Max Thrust: 102,2 N
Engine Average Thrust: 102,2 N
Engine Full Impulse: 684,8 Ns
Rocket Velocity at the Top of the Launch Platform: 17,8 m/s
Altitude record 965 m, at Rovajärvi 6.9.2008
Webmaster of this site: Aapo Puhakka