Development of uncooled nozzles for missiles and space boosters requiring nozzle of large throat diameter to withstand gas temperature greater than 3200 K for 3 min for first stage and expansion cone of small dimensions to meet gas temperature of 1500 K under conditions of high heat transfer since liquid hydrogen will be fuel for third stage; mechanisms responsible for nozzle failure; testing of nozzle materials. Abstract of paper before meeting Nov 22 1961 of Brit Interplanetary Soc.
Rocket nozzle development
Aeroplane Astronautics
Aeroplane and Astronautics ; 102 , n 2620
1962
3 pages
Article (Journal)
English
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