All this information pertains to
12" X 1" PVC rocket engines, 0.25" throat,
Kn = 288
propellant weight = 0.22 Kg
Isp = 190 N/S
Formulation:
Kn
Kp
epoxy
Iron Oxide
Zn
Video: lanzamiento.mov (1.17 Mb)
Static test report for TM1202 by Hans Olaf Toft
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. |