Malewicki Equations
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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]
[edit] References
- ^ Model Rocket Altitude Prediction Charts Including Aerodynamic Drag, Douglas J. Malewicki, Technical Report No. TR-10, Estes Industries, Inc., Penrose, Colorado, USA, 1967
- ^ [http://www.la.unm.edu/~beach/altitudeHelp1.html Documentation for Altitude Applet (see "Equations" section)
