Ascent trajectory dispersion analysis
Abstract
The results of a Space Transportation System ascent trajectory dispersion analysis are documented. Critical trajectory parameter values useful for the definition of lightweight external tank insulation requirements are provided. This analysis was conducted using two of the critical missions specified for the Space Transportation System: a 28.5 deg inclination trajectory launched from the Eastern Test Range (ETR) and a Western Test Range (WTR) trajectory launched into a 104 deg orbital inclination.
- Publication:
-
Final Report Dynetics
- Pub Date:
- December 1982
- Bibcode:
- 1982dyni.rept......
- Keywords:
-
- Ascent Trajectories;
- Dispersions;
- External Tanks;
- Parameter Identification;
- Space Transportation System;
- Trajectories;
- Astrodynamics