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53T6: Revision history

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27 May 2024

  • curprev 00:0400:04, 27 May 2024‎ 2003:e3:8f22:3b45:594d:1b40:df75:a83b talk‎ 6,511 bytes −40‎ corrected false information.high thrust (and thus high acceleration) is not correlated with high specifoc impulse. in fact those engines with the highest isp usually have a very low thrust to mass ratio (for example ion engines) and vice versa (example: solid fuel chemi cal rockets, the type most likely used in this particular missile) undo

20 April 2024

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