File:Engine thrust to weight.png
Engine_thrust_to_weight.png (400 × 300 pixels, file size: 4 KB, MIME type: image/png)
Graph representing rocket dry and wet mass as function of the engine's thrust-to-weight ratio.
Click on a date/time to view the file as it appeared at that time.
|current||22:08, 11 December 2012||400 × 300 (4 KB)||Vincent||Updated with version 3 of File:Rocket_mass.c. Delta V is 8300 instead of 9000 m/s too, and overall thrust-to-weight ratio is 2.5 instead of 1.25.|
|06:45, 1 November 2012||400 × 300 (4 KB)||Vincent||Graph representing rocket dry and wet mass as function of the engine's thrust-to-weight ratio.|
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