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PROPELLANT BURN TIME [1 record]

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Record 1 2004-02-12

English

Subject field(s)
  • Launchers (Astronautics)
CONT

The two solid boosters each contain 9. 5 metric tons of solid propellant, and develop 625 kN of thrust(140, 500 lb), with a burn time of 34 seconds.

French

Domaine(s)
  • Lanceurs (Astronautique)
CONT

Finalement, le GSLV emploiera tout de suite les moteurs d'appoint à Vikas de basse altitude (Viking 2). Mais ce ne sont pas à proprement parler des boosters : leur temps de combustion dépasse celui du premier étage.

Spanish

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