curprev14:4314:43, 3 November 2020 AristosMtalkcontribs m44,625 bytes+12 Change relative time reference into absolute time reference. The original "30 years" was written in 2004, so the absolute date is the mid-1970s.undo
curprev14:3114:31, 15 April 2019 Gah4talkcontribs 43,873 bytes−36 →Early development, 1926: remove {{citation needed|date=March 2017}} . I think everyone knows that gasoline is readily available, cheap, and highly energetic. Slightly less obvious for LOX, but only slightly. If it needs more, ask on Talk.undo
curprev04:2004:20, 21 June 2018 Jamescookmdtalkcontribs 42,428 bytes+198 Added reference for V-2 rocket fuels. A paperback version of the book "Ignition!" was recently published and might contain other useful references for this article.undo
17 May 2018
curprev15:0915:09, 17 May 2018 Antwan718talkcontribs m42,230 bytes+13 →Monopropellants: Previously stated that ammonia decomposition would decrease rocket engine performance. From free enthalpy calculations, this claim is true only if there is no oxidizer present. The text has been modified to be less missleading.undo
curprev02:0102:01, 1 July 2006 80.177.20.202talk 42,349 bytes−6 this is ridiculous. who writes this stuff? this is an encylopedia, and people are typing entries as though it were a gossip column in some trashy magazine. for goodness sake.undo
curprev15:4115:41, 16 August 2005 Wolfkeepertalkcontribs 42,126 bytes+96 I don't like noted; it implies correctness-no propellant is ideal-low mass is the primary advantage of hydrogen upper stages, hydrogen in gaseous form can be used, but does not give a high mass ratioundo