This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Concept for a Large Multipurpose Launch Vehicle
Annotation ability available
Sector:
Event:
Space Technology Conference
Language:
English
Abstract
The key results of a NASA-sponsored study of a large multipurpose launch concept are summarized. The study evolved, through parametric performance and detailed design analyses, the characteristics of an attractive launch vehicle approach for consideration in future mission planning studies. The reported vehicle system has only two stages: a LOX/LH2 main stage and a solid-motor strap-on stage. The main stage has the performance capability to fly single-stage-to-orbit and the structural capability to accommodate strap-on stages to achieve a broad range of payload flexibility. The salient features of the vehicle system, sized to deliver one to four million pounds to low earth orbit, are described. The major resource and technology implications of the system are discussed.
Recommended Content
Technical Paper | Distributed Planning In The Rapid Product Development Using Adaptable Process Modules |
Technical Paper | Capacity Planning and Productivity—A Tutorial |
Book | Managing Complexity |
Citation
Gomersall, E. and Brunk, J., "Concept for a Large Multipurpose Launch Vehicle," SAE Technical Paper 680356, 1968, https://doi.org/10.4271/680356.Also In
References
- The Boeing Co., “Study of Advanced Multipurpose Large Launch Vehicles - Summary Report (U).” NASA Contract NAS2-4079, NASA CR-73154 1968
- The Boeing Co., “Study of Advanced Multipurpose Large Launch Vehicles - Technical Report (U).” NASA Contract NAS2-4079, NASA CR-73155 1968