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THRUST WEIGHT RATIO [1 record]

Record 1 2001-02-15

English

Subject field(s)
  • Aircraft Propulsion Systems
DEF

Engine thrust divided by aircraft weight.

CONT

The thrust to weight ratio is an efficiency factor for total aircraft propulsion. An aircraft with a high thrust to weight ratio has high acceleration. It has a high value of excess thrust which results in a high rate of climb.

French

Domaine(s)
  • Propulsion des aéronefs
CONT

Le M88-2 est entièrement conçu, développé et fabriqué par Snecma. Par sa conception modulaire, son rapport masse/poussée, ses capacités d'accélération et sa pilotabilité exceptionnelles, il se place au meilleur niveau technologique mondial.

Spanish

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