Malewicki Equations

The Malewicki Equations (or Fehskens-Malewicki Equations) for Sub-sonic Endo-atmospheric Rocket Flight describe the maximum altitude and coast time of a vehicle such as a model rocket. Aerospace engineer and inventor Douglas Malewicki first published them as a technical report by the model rocket company Estes Industries in 1967. ^{[1] [2]}

References

1. ^ Model Rocket Altitude Prediction Charts Including Aerodynamic Drag, Douglas J. Malewicki, Technical Report No. TR-10, Estes Industries, Inc., Penrose, Colorado, USA, 1967
2. ^ Documentation for Altitude Applet (see "Equations" section)