The study objective is to characterize the performance capabilities of an inline, shuttle-derived launch vehicle using two design strategies: the first as an early program demonstrator utilizing high structural margins, maximum shuttle assets, and minimal pad impact, the later having undergone structural optimization, flying operational mission GR&A and serving as a baseline for evolutionary upgrades.
Launch Vehicle Demonstrator Using Shuttle Assets
2011
12 pages
Report
No indication
English
Launch Vehicle Demonstrator Using Shuttle Assets
NTIS | 2011
|Launch Vehicle Demonstrator Using Shuttle Assets
NTRS | 2011
|Launch Vehicle Demonstrator Using Shuttle Assets
AIAA | 2011
|Launch Vehicle Demonstrator Using Shuttle Assets
NTRS | 2011
|Launch Vehicle Demonstrator Using Shuttle Assets
British Library Conference Proceedings | 2011
|