Review of development trends for solid propellant rockets of over 1, 000,000 lb thrust considers case and nozzle design and requirements for propellants, materials, and fabrication; partial tests, while yielding significant data, help conserve costly propellant and case material.
Solids competitive for multi-million-pound boosters
Space/Aeronautics
Space/Aeronautics ; 34 , n 4
1960
3 pages
Article (Journal)
English
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