by Hans Olaf Toft
Test conducted 28-06-2002 17:52 at Stold
Propellant:
Propellant Weight: 0.695 kg
Average Propellant Density: 1687.850 kg/m³
Composition:
8.3% H85
16.6% A1000
2% Al
2% C
46% KNO3
25% KCLO4
Nozzle Dimensions:
Diameter of Nozzle Throat: 9.50 mm
Diameter of Nozzle Exit: 14.00 mm
Length of Nozzle Expansion Cone: 10.00 mm
Estimated Performance
Total Impulse: 562.41 Ns (Class I)
Average Specific Impulse: 114.39441 s
c*: 916.97225 m/s
Grain 1 Drawing
NedStat:
| Contents of this web page is presented for informational purposes only. Author of this web site cannot assume responsibility for the use readers make of the information presented herein or the devices resulting therefrom. Amateur Experimental Rocketry has many inherent hazards that must be fully understood before one can consider becoming actively involved. Safety must always be considered as top priority. Anything less is a disservice to all Amateur Experimental Rocketry enthusiasts. If you do not have first-rate common sense, or if you are willing to take shortcuts that compromise safety, then Amateur Experimental Rocketry is not for you. |