Talk:HAL HF-24 Marut
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[edit]The only things keeping this one from being directly tagged as a stub are the various tables - as (1) the first indiginous Indian military aircraft and (2) the last of the Kurt Tank (= Focke-Wulf) line, this is a more important subject than your average bear, and deserves some attention from those knowedgable on the subject. - Aerobird 04:20, 16 December 2006 (UTC)
War history
[edit]The fighter did see action in the Indo-pakistan war of 1971. The details should be mentioned.
I do remember this page being bigger, or maybe theres another, bigger Marut page on wikipedia...This page can defnitely be expanded by leaps and bounds.. theres a lot more information available than is shown here. 155.69.5.236 07:08, 28 March 2007 (UTC)
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[edit]This article was automatically assessed because at least one WikiProject had rated the article as stub, and the rating on other projects was brought up to Stub class. BetacommandBot 18:05, 9 November 2007 (UTC)
Assessment comment
[edit]The comment(s) below were originally left at Talk:HAL HF-24 Marut/Comments, and are posted here for posterity. Following several discussions in past years, these subpages are now deprecated. The comments may be irrelevant or outdated; if so, please feel free to remove this section.
Needs infobox, references. Specifications and footer are complete. Also, needs much more text. As a contemporary aircraft, there is surely a wealth of information available on its development and use. Karl Dickman talk 01:21, 11 January 2007 (UTC) |
Last edited at 01:21, 11 January 2007 (UTC). Substituted at 16:55, 29 April 2016 (UTC)
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HF-24 MARUT Rate of Climb 22.5 m/s or 4,444 ft/min
[edit]In Performance section rate of climb should be 22.5 ms or 4,444 ft/min
Why? because it is Accurate performance data obtained from IAF evaluation, that can be check all over internet or in any book ! Also if someone calculate "Time to altitude": 9 min 20 s to 12,000 m (40,000 ft) to m/s or ft/min it will get the same results !
Max climb rate - 22.5 ms (4,444ft/min) — Preceding unsigned comment added by TRUTH, JUSTICE & RIGHT WAY (talk • contribs) 05:19, 18 January 2020 (UTC)
- 1) You don't get the same results - 12000/560 = 21.4 m/s. not 22.5. 2) You cannot convert Time to altitude to an climb rate by simple division, as the climb rate is the maximum, instantaneous figure (normally at sea level) - this maximum would be expected to be much higher then the average value given by a time to altitude. 3) If the values you quote are "all over the internet" or "in any book", where are they? The only source that you quoted, militaryfactory.com is not a reliable source - while Jane's All the World's Aircraft is a high quality reliable source (who would have got their information from HAL or the Indian government). Please provide sources or revert.Nigel Ish (talk) 11:26, 18 January 2020 (UTC)
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