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
37 pages
Report
No indication
English
Unmanned Spacecraft , Spacecraft Trajectories & Flight Mechanics , Astronautics , Orbit transfer vehicles , Trajectory analysis , Computation , Mission planning , Numerical analysis , Aerobraking , Avionics , Graphs (Charts) , Spacecraft propulsion , Spacecraft structures , Spacecraft trajectories , Tables (Data)