User:Milton Beychok/Sandbox: Difference between revisions

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==Rocket thrust and specific impulse==
==Rocket thrust and specific impulse==


Thrust is the [[force]] ('''''F''''')  which moves a rocket through the air. Thrust is generated by the rocket engine through the reaction  of [[acceleration|accelerating]] a mass of gas. The gas is accelerated to the the rear by the venturi effect of the deLaval nozzle and the rocket is accelerated in the opposite direction. Force may be mathematically expressed as:<ref>[http://exploration.grc.nasa.gov/education/rocket/specimp.html Specific Impulse] from a website page of [[National Aeronautics and Space Administration]] (NASA)<ref>
Thrust is the [[force]] ('''''F''''')  which moves a rocket through the air. Thrust is generated by the rocket engine through the reaction  of [[acceleration|accelerating]] a mass of gas. The gas is accelerated to the the rear and the rocket is accelerated in the opposite direction. Force may be mathematically expressed as:<ref>[http://exploration.grc.nasa.gov/education/rocket/rktthsum.html Rocket Thrust Summary] from a website page of the [[National Aeronautics and Space Administration]] (NASA)</ref><ref>[http://exploration.grc.nasa.gov/education/rocket/specimp.html Specific Impulse] from a website page of the National Aeronautics and Space Administration (NASA)</ref>


:<math>F = \dot {m} V_e + (p_e - P_0)A_c</math>
:<math>F = \dot {m} V_e + (p_e - P_0)A_c</math>


and also this form (by defining a new term '''''v<sub>eq</sub>'''''&thinsp;:
and also this form, by defining a new term '''''v<sub>eq</sub>'''''&thinsp;:


:<math>F = \dot {m} V_{eq} = \dot {m} \left [V_e + \frac {(p_e - P_0)A_c}{\dot {m}} \right ]</math>
:<math>F = \dot {m} V_{eq} = \dot {m} \left [V_e + \frac {(p_e - P_0)A_c}{\dot {m}} \right ]</math>

Revision as of 16:05, 24 March 2010

Rocket thrust and specific impulse

Thrust is the force (F) which moves a rocket through the air. Thrust is generated by the rocket engine through the reaction of accelerating a mass of gas. The gas is accelerated to the the rear and the rocket is accelerated in the opposite direction. Force may be mathematically expressed as:[1][2]

and also this form, by defining a new term veq :


  1. Rocket Thrust Summary from a website page of the National Aeronautics and Space Administration (NASA)
  2. Specific Impulse from a website page of the National Aeronautics and Space Administration (NASA)