Abstract This chapter provides a general description of propulsion systems suitable for missiles. These systems are solid- and liquid-fuelled rockets, liquid-fuelled ramjets, solid fuel ducted rockets (ramrockets), and scramjets. Concise summaries about testing are also given, and mention is made of a scramjet test facility developed by the Defence Research and Development Laboratory (DRDL) in Hyderabad, India. This facility is part of the DRDL hypersonic programme entitled ‘Hypersonic Technology Demonstrator Vehicle’ (HSTDV).
Missile Propulsion Systems
08.11.2016
26 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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