Template:Specific impulse examples

Specific impulse of different ways to push a rocket
Engine Effective exhaust velocity
(m/s, kg·m/s/kg) 		Specific impulse
(s) 		Energy per kg of exhaust
(MJ/kg)
Turbofan jet engine
(actual V is ~300) 		29,000 3,000 ~0.05    
Solid fuel rocket 2,500 250 3    
Liquid fuel rocket 4,400 450 9.7    
Ion thruster 29,000 3,000 430    
Dual Stage Four Grid Electrostatic Ion Thruster [1] 210,000 21,400 22,500    
VASIMR [2][3][4] 30,000-120,000 3,000-12,000 1,400    


References

These references will appear in the article, but this list appears only on this page.
  1. ↑ "kernel (1)". www.esa.int. Archived from the original on December 8, 2022. Retrieved Mar 3, 2023.
  2. ↑ "Principal VASIMR Results and Present Objectives" (PDF). Archived from the original (PDF) on 2007-01-09. Retrieved 2011-09-04.
  3. ↑ "VASIMRR Performance Results" (PDF). Archived from the original (PDF) on 2020-08-07. Retrieved 2011-09-04.
  4. ↑ "Vasimr VX-200 meets full power efficiency milestone". Archived from the original on 2017-03-30. Retrieved 2011-09-04.

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