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- W2074872922 abstract "The Institute of Space and Astronautical Science (ISAS) is undertaking development of its newest satellite launcher, M-V. HTPB-based highly aluminized composite propellents have been developed, and the subatmospheric burning rate characteristics of these propellents were investigated to properly anticipate the thrust decay behavior into the residual thrust region of each stage motor. A simple but unique method was employed in the measurements. The size of the propellent specimen was quite small; 8 mm long and 8 mm in diameter. Ignition was detected by a photo-transistor, and burnout by an ion probe or a fine thermocoupie." @default.
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- W2074872922 date "1994-01-01" @default.
- W2074872922 modified "2023-09-26" @default.
- W2074872922 title "STUDY ON THE SUBATMOSPHERIC BURNING RATE CHARACTERISTICS OF COMPOSITE PROPELLANTS" @default.
- W2074872922 doi "https://doi.org/10.1615/intjenergeticmaterialschemprop.v3.i1-6.600" @default.
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