Unmanned, Space-Based, Reusable Orbital Transfer Vehicle, Darves. Volume 2. Data and Calculations

摘要

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.