Differences between revisions 3 and 4

Rocket Engines

Contemplating the expansion ratio and mach number of miscellaneous high-expansion rocket engines. The mach number is from Figure 3.1 on page 39, assuming a specific heat ratio of 1.3:

	ratio	mach
Saturn V first stage F1	16.1	4.01
Saturn V 2nd/3rd J2	27.5	4.50
Apollo SM AJ10-137	62.5	5.31
Shuttle SSME RS-25	77.5	5.53
SpaceX Merlin Vacuum 1C	14.5	3.91
SpaceX Merlin Vacuum 1D	165	6.36

Laser Ablation Thrust	2.95	2.50

-  ⇤ ← Revision 3 as of 2019-06-13 23:05:58 → 
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+   ← Revision 4 as of 2019-06-15 17:38:23 → ⇥
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Diff for "RocketEngines"

Rocket Engines