 | A fact from Lockheed J37 appeared on Wikipedia's Main Page in the Did you know column on 9 February 2008, and was viewed approximately 2,811 times (disclaimer) (check views). The text of the entry was as follows:
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Thrust edit
There is a discrepancy with the value given for thrust of 5,100 lbf (2,315 N). 5,100lbf actually equals 22700N, while 2315N equals 520lbf. 5,100lb equals 2313kg - perhaps this is where the error lies? Given the thrust range of comparable engines from the period, I'd suspect 5,100lbf is the correct thrust, and I have amended the article accordingly. If someone could provide a sourced answer to this question though, that would be useful. --Nick Moss (talk) 12:07, 24 February 2009 (UTC)
Efficiency edit
Why was it felt that the engine's efficiency had to be comparable to a piston-engine? I don't think any turbojet engine of that era could come even close at low altitudes (If they even can now). AVKent882 (talk) 02:56, 29 October 2010 (UTC)