Results for trajectory analysis, fuel analysis, and analysis of aerobraking maneuvers are presented. Calculations are included for thickness and mass of the propellant tanks; determination of weight (avionics module); numerical integration program; hydrostatic pressure due to acceleration; and propellant tank pressurization.
Unmanned, space-based, reusable orbital transfer vehicle, DARVES. Volume 2: Data and calculations
1988-06-01
Report
No indication
English