词条 | Malewicki equations |
释义 |
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]References1. ^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) {{webarchive|url=https://web.archive.org/web/20071210032718/http://www.la.unm.edu/~beach/altitudeHelp1.html#assume |date=2007-12-10 }} 1 : Aerospace engineering |
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