[1] viXra:1509.0133 [pdf] submitted on 2015-09-15 14:32:22
Authors: Oliver R Jovanovic
Comments: 5 Pages.
Note that in "Airfoil force approach", force (rocket thrust) has quadratic dependence on the velocity.
This quadratic dependence on the velocity is giving us opportunity to reduce rate of mass ejection (fuel loss).
Category: Thermodynamics and Energy