Theoretical Analysis of Dual-Thrust Rocket Motors with Intermediate Nozzle
Date
2017
Journal Title
Journal ISSN
Volume Title
Type
Article
Publisher
AMER INST AERONAUTICS ASTRONAUTICS
Series Info
JOURNAL OF PROPULSION AND POWER;Volume: 33 Issue: 2 Pages: 531-536
Doi
Scientific Journal Rankings
Abstract
Description
Accession Number: WOS:000395741800026
Keywords
University for Modern Sciences and Arts
Citation
Cited References in Web of Science Core Collection: 10