Weights assessment for orbit-on-demand vehicles
Abstract
Future manned, reusable earth-to-orbit vehicles may be required to reach orbit within hours or even minutes of a mission decision. A study has been conducted to consider vehicles with such a capability. In the initial phase of the study, 11 vehicles were sized for deployment of 5000 lbs to a polar orbit. From this matrix, two of the most promising concepts were resized for a modified mission and payload. A key feature of the study was the use of consistent mass estimating techniques for a broad range of concepts, allowing direct comparisons of sizes and weights.
- Publication:
-
Society of Allied Weight Engineers
- Pub Date:
- May 1985
- Bibcode:
- 1985sawe.conf.....M
- Keywords:
-
- Expendable Stages (Spacecraft);
- Orbit Transfer Vehicles;
- Orbital Launching;
- Payloads;
- Reusable Launch Vehicles;
- Avionics;
- Bending Moments;
- Environmental Control;
- Hydrocarbon Fuels;
- Landing Gear;
- Liquid Hydrogen;
- Liquid Oxygen;
- Propellant Tanks;
- Propulsion System Configurations;
- Launch Vehicles and Space Vehicles