Development and Testing of a Two-Stage Hybrid Launcher.
Abstract
This report summarizes the development to date of a 1/4-scale launcher designed to launch a 7.2-kg model at a 6.1 km/sec in full scale. The hybrid launcher design principles are reviewed. Projected performance shows launch masses within soft-launch constraints that are 3 to 4 times larger than possible by using a conventional two-stage launcher. The results of component development tests leading to the subscale demonstration are presented. The importance of tungsten liners for obtaining the projected performance is emphasized, and the results of liner bond developments are described. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 31, 1979
- Accession Number
- ADA086268
Entities
People
- J. D. Watson
- J. L. Hull
- K. E. Suchsland
- T. J. Dahm