The thrust developed by a rocket–motor is given by F = mv + A(p 1 – p 2 ), where m is the…

Physics · JEE Main · NTA ExamsPhysics and Measurement

The thrust developed by a rocket–motor is given by F = mv + A(p1 – p2), where m is the mass of the gas ejected per unit time, v is velocity of the gas, A is area of cross–section of the nozzle, p1, p2 are the pressures of the exhaust gas and surrounding atmosphere. The formula is dimensionally
  1. Correct
  2. Wrong
  3. Sometimes wrong, sometimes correct
  4. Data is not adequate

Answer

(A) Correct

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