Thermal Reactivity of Double‐Base Rocket Propellants | Zendy

Pai Verneker V. R. | Zendy; Kishore K. | Zendy; Subhas C. B. V. | Zendy

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Thermal Reactivity of Double‐Base Rocket Propellants

Author(s) -

Pai Verneker V. R.,

Kishore K.,

Subhas C. B. V.

Publication year - 1979

Publication title -

propellants, explosives, pyrotechnics

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.56

H-Index - 65

eISSN - 1521-4087

pISSN - 0721-3115

DOI - 10.1002/prep.19790040406

Subject(s) - thermal decomposition , propellant , thermogravimetric analysis , rocket (weapon) , decomposition , base (topology) , materials science , double bond , reactivity (psychology) , thermal , chemistry , analytical chemistry (journal) , aerospace engineering , thermodynamics , polymer chemistry , organic chemistry , physics , engineering , medicine , mathematical analysis , alternative medicine , mathematics , pathology

Thermal decomposition studies on double‐base propellants have been carried out in air and vacuum using differential scanning calorimetric, thermogravimetric and mass spectrometric techniques. Low temperature (90 °C–170 °C) decomposition seems to involve diffusion controlled process, the mechanism in air and vacuum being different. High temperature (170 °–205 °C) decomposition involves bond breakage.

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