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&lt;p&gt;&lt;b&gt;New page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;{{Short description|1961 fighter aircraft family by Hindustan Aircraft Limited}}&lt;br /&gt;
&amp;lt;!-- This article is a part of [[Project:WikiProject Aircraft]]. Please see [[Project:WikiProject Aircraft/page content]] for recommended layout. --&amp;gt;&lt;br /&gt;
{|{{Infobox aircraft begin&lt;br /&gt;
 |name = HF-24 Marut&lt;br /&gt;
 |image = File:HAL (Hindustan Aeronautics), HF-24, Marut (7585415088).jpg&lt;br /&gt;
 |caption =&lt;br /&gt;
}}{{Infobox aircraft type&lt;br /&gt;
 |type = [[Fighter-bomber]]&lt;br /&gt;
 |manufacturer = [[Hindustan Aeronautics Limited]]&lt;br /&gt;
 |national origin=India&lt;br /&gt;
 |designer = [[Kurt Tank]]&lt;br /&gt;
 |first flight = 17 June 1961&lt;br /&gt;
 |introduced = 1 April 1967&lt;br /&gt;
 |retired = 1990&lt;br /&gt;
 |produced =&lt;br /&gt;
 |number built = 147&amp;lt;ref name=&amp;quot;Donald World p523&amp;quot;&amp;gt;Donald 1997, p. 523.&amp;lt;/ref&amp;gt;&lt;br /&gt;
 |status =&lt;br /&gt;
 |primary user = [[Indian Air Force]]&lt;br /&gt;
 |more users = &lt;br /&gt;
 |developed from =&lt;br /&gt;
 |variants with their own articles = &lt;br /&gt;
}}&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
The &amp;#039;&amp;#039;&amp;#039;HAL HF-24 Marut&amp;#039;&amp;#039;&amp;#039; (&amp;quot;Spirit of the Tempest&amp;quot;) was an Indian [[fighter-bomber]] [[aircraft]] of the 1960s. Developed by [[Hindustan Aeronautics Limited]] (HAL), with [[Kurt Tank]] as lead designer. The Project Engineer from [[Hindustan Aeronautics Limited|HAL]] was George William Benjamin. It is the first Indian-developed jet aircraft, and the first [[Asia]]n jet [[Fighter aircraft|fighter]] (outside Russia/Soviet Union) to go beyond the test phase and into successful production and active service. On 17 June 1961, the type conducted its [[maiden flight]]; on 1 April 1967, the first production Marut was officially delivered to the IAF.&lt;br /&gt;
&lt;br /&gt;
While the Marut had been envisioned as a [[supersonic]]-capable combat aircraft, it would never manage to exceed [[Mach number|Mach 1]]. This limitation was principally due to the engines used, which in turn had been limited by various political and economic factors; multiple attempts to develop improved engines or to source alternative powerplants were fruitless. The Marut&amp;#039;s cost and lack of capability in comparison to contemporary aircraft were often criticised.&lt;br /&gt;
&lt;br /&gt;
A total of 147 Maruts were manufactured, the majority for the [[Indian Air Force]] (IAF). While initially envisioned as a capable [[interceptor aircraft]], it was primarily used for ground attack missions. In this role, the Marut saw combat during the [[Indo-Pakistani War of 1971]], notably participating in the [[Battle of Longewala]]. By 1982, the Marut was increasingly obsolescent, and was gradually phased out during the late 1980s.&lt;br /&gt;
&lt;br /&gt;
==Design and development==&lt;br /&gt;
===Origins===&lt;br /&gt;
During the 1950s, Hindustan Aircraft Limited (HAL) had developed and produced several types of trainer aircraft, such as the [[HAL HT-2]]. However, elements within the firm were eager to expand into the then-new realm of supersonic fighter aircraft.&amp;lt;ref name = &amp;quot;sat 480&amp;quot;&amp;gt;Satish 2015, p. 480.&amp;lt;/ref&amp;gt; Around the same time, the Indian government was in the process of formulating a new Air Staff Requirement for a Mach 2-capable combat aircraft to equip the Indian Air Force (IAF).&amp;lt;ref name = &amp;quot;gupta 34&amp;quot;&amp;gt;Gupta 1997, p. 34.&amp;lt;/ref&amp;gt; However, as HAL lacked the necessary experience in both developing and manufacturing frontline combat fighters, it was clear that external guidance would be invaluable; this assistance was embodied by [[Kurt Tank]].&lt;br /&gt;
&lt;br /&gt;
In 1956, HAL formally began design work on the supersonic fighter project.&amp;lt;ref name = &amp;quot;smith 160&amp;quot;&amp;gt;Smith 1994, p. 160.&amp;lt;/ref&amp;gt;&amp;lt;ref name = &amp;quot;sat 480&amp;quot;/&amp;gt; The Indian government, led by [[Jawaharlal Nehru]], authorised the development of the aircraft, stating that it would aid in the development of a modern aircraft industry in India.&amp;lt;ref name = &amp;quot;Rajagopalan 116&amp;quot;&amp;gt;Rajagopalan 2014, p. 116.&amp;lt;/ref&amp;gt; The first phase of the project sought to develop an airframe suitable for travelling at supersonic speeds, and able to effectively perform combat missions as a fighter aircraft, while the second phase sought to domestically design and produce an engine capable of propelling the aircraft.&amp;lt;ref name = &amp;quot;smith 160&amp;quot;/&amp;gt; Early on, there was an explicit adherence to satisfying the IAF&amp;#039;s requirements for a capable fighter bomber; attributes such as a twin-engine configuration and a speed of Mach 1.4 to 1.5 were quickly emphasised.&amp;lt;ref name = &amp;quot;smith 160&amp;quot;/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
During development, HAL designed and constructed a full-scale two-seat wooden glider to act as a flying demonstrator. Designated &amp;#039;&amp;#039;HAL X-241&amp;#039;&amp;#039;, this replicated production aircraft in terms of dimensions, control configuration, and aerofoil sections. The wheel brakes, air brakes, flaps, and retractable undercarriage were all actuated using compressed gas, with sufficient gas storage aboard for multiple actuations per flight.&amp;lt;ref name=Bhargava&amp;gt;{{cite web|last1=Bhargava|first1=Kapil, Gp.Capt. (retd.)|title=The HF-24 Marut&amp;#039;s Glider Prototype|url=http://www.bharat-rakshak.com/IAF/History/1950s/Kapil-Glider.html|website=bharat-rakshak.com|access-date=10 June 2014|url-status=dead|archive-url=https://web.archive.org/web/20150407084138/http://www.bharat-rakshak.com/IAF/History/1950s/Kapil-Glider.html|archive-date=7 April 2022}}&amp;lt;/ref&amp;gt; On 3 April 1959, the X-241 flew for the first time, having been launched by aero-tow behind a [[Douglas DC-3|Douglas Dakota Mk.IV]] BJ 449. A total of 86 flights were conducted prior to the X-241 receiving considerable damage as the result of a landing accident, after the nose undercarriage failed to extend.&amp;lt;ref name=Bhargava/&amp;gt;&amp;lt;ref name = &amp;quot;times india 2016&amp;quot;/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
On 24 June 1961, the first prototype Marut conducted its maiden flight.&amp;lt;ref name = &amp;quot;gupta 34&amp;quot;/&amp;gt;&amp;lt;ref name = &amp;quot;times india 2016&amp;quot;/&amp;gt; It was powered by the same [[Bristol Siddeley Orpheus]] 703 [[turbojet]]s that had powered the [[Folland Gnat]], also being manufactured by HAL at that time. On 1 April 1967, the first production Marut was delivered to the IAF.&amp;lt;ref name = &amp;quot;times india 2016&amp;quot;&amp;gt;Singh, Sushant. [http://indianexpress.com/article/explained/tejas-light-combat-aircraft-indigenous-india-iaf-hf-24-2887950/ &amp;quot;Tejas is not India&amp;#039;s first indigenous fighter, that would be the HF-24 Marut.&amp;quot;] &amp;#039;&amp;#039;Times of India&amp;#039;&amp;#039;, 1 July 2016.&amp;lt;/ref&amp;gt; While originally intended only as an interim measure during testing, HAL decided to power production Maruts with a pair of [[afterburner|unreheated]] Orpheus 703s, meaning the aircraft could not attain supersonic speed.&amp;lt;ref name = &amp;quot;gupta 34&amp;quot;/&amp;gt; Although originally conceived to operate around Mach 2, the Marut in fact was barely capable of reaching Mach 1 due to the lack of suitably powerful engines.&amp;lt;ref name = &amp;quot;gupta 34&amp;quot;/&amp;gt;&amp;lt;ref name=&amp;quot;fas_marut_supersonic&amp;quot;&amp;gt;{{cite web|url=http://www.fas.org/man/dod-101/sys/ac/row/marut.htm|publisher=Federation of American Scientists|title=HF-24 Marut}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
The IAF were reluctant to procure a fighter aircraft only marginally superior to its existing fleet of British-built [[Hawker Hunter]]s; however, in 1961, the Indian Government decided to procure 16 pre-production and 60 production Maruts.&amp;lt;ref name = &amp;quot;times india 2016&amp;quot;/&amp;gt; Only 147 aircraft, including 18 two-seat trainers, were completed out of a planned 214.&amp;lt;ref name = &amp;quot;gupta 34&amp;quot;/&amp;gt; After the Indian Government conducted its first [[nuclear tests]] at [[Pokhran]], international pressure prevented the import of better engines, or at times, even spares for the Orpheus engines; this situation was one of the main reasons for the aircraft&amp;#039;s early demise. The Marut never realised its full potential due to insufficient power. The Marut &amp;quot;was technically obsolete by the time it was first delivered in 1964&amp;quot;.&amp;lt;ref name = &amp;quot;gupta 34&amp;quot;/&amp;gt; Other authors have also commented on the Marut&amp;#039;s relative obsolescence by the time it reached production.&amp;lt;ref&amp;gt;Arnett 1997, pp. 120–121.&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
===Termination and criticisms===&lt;br /&gt;
The Marut was described as &amp;quot;essentially a very long-drawn-out failure&amp;quot;, and the aircraft&amp;#039;s shortcomings were considered to be due to multiple factors.&amp;lt;ref name = &amp;quot;smith 160 161 162&amp;quot;&amp;gt;Smith 1994, pp. 160–162.&amp;lt;/ref&amp;gt; Among these were the difficulties experienced in securing a suitable engine, which was principally a political issue; while arrangements were successfully established with the United Kingdom and [[Bristol Siddeley]] for HAL to domestically produce the Orpheus, it was only suitable as an interim measure as it lacked the power to enable the Marut to achieve supersonic speed.&amp;lt;ref name = &amp;quot;smith 160 161&amp;quot;&amp;gt;Smith 1994, pp. 160–161.&amp;lt;/ref&amp;gt; The Indian Government refused a proposal made by [[Rolls-Royce Ltd|Rolls-Royce]] to finance further development of the Orpheus, which had been specifically aimed at producing a more suitable engine for the Marut.&amp;lt;ref name = &amp;quot;smith 160 161&amp;quot;/&amp;gt;&amp;lt;ref name = &amp;quot;gupta 34&amp;quot;/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Other envisioned alternative engines that might have been sourced from the Soviet Union, Egypt, or various European nations did not result in anything of substance.&amp;lt;ref name = &amp;quot;gupta 34&amp;quot;/&amp;gt;&amp;lt;ref name = &amp;quot;smith 161&amp;quot;/&amp;gt; The [[Gas Turbine Research Establishment]] also pursued their own development program to improve the Orpheus without external aid, which proceeded to the testing phase with some favourable results, but proved incompatible with the Marut.&amp;lt;ref name = &amp;quot;arnett 120&amp;quot;/&amp;gt; As the particularities of a given airframe are typically heavily dependent on the engine used, the inability to improve the Marut&amp;#039;s powerplant damaged its performance.&amp;lt;ref name = &amp;quot;smith 161&amp;quot;&amp;gt;Smith 1994, p. 161.&amp;lt;/ref&amp;gt; Despite experimentation with various engines, the Marut was never able to achieve supersonic speeds, which was viewed as a major failure.&amp;lt;ref name = &amp;quot;smith 160&amp;quot;/&amp;gt; IAF had anticipated the Marut being fitted with a considerably superior engine.&amp;lt;ref name = &amp;quot;arnett 120&amp;quot;/&amp;gt;&amp;lt;ref&amp;gt;Thomas 2014, p. 260.&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
The project was negatively affected by a lack of direction and management from the [[Ministry of Defence (India)|Indian Ministry of Defence]].&amp;lt;ref name = &amp;quot;smith 161&amp;quot;/&amp;gt; A lack of coordination between the military, politicians, and industry is alleged to have been typical throughout the entirety of the programme, leaving many issues down to industry alone without guidance. Specifically, the government never sanctioned the development of an engine design team, nor were there assessments of HAL&amp;#039;s capability to [[reverse engineer]] or to apply technologies from other projects, such as the work performed for the Folland Gnat.&amp;lt;ref name = &amp;quot;smith 162&amp;quot;/&amp;gt; HAL is claimed to have struggled to convince both the IAF and MoD that the design of the Marut was acceptable; much attention was given to the unacceptably high level of trail drag{{clarify|date=August 2022}} the airframe produced, as well as dissatisfaction with the Marut&amp;#039;s speed and manoeuvrability, both of which were below IAF specification upon the aircraft&amp;#039;s introduction.&amp;lt;ref name = &amp;quot;smith 161&amp;quot;/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Tank had a major influence on the project, and accordingly of its shortcomings. While working on the Marut, he was criticized for a rigid stance on aspects of the design,&amp;lt;ref name = &amp;quot;smith 160 162&amp;quot;&amp;gt;Smith 1994, pp. 160, 162.&amp;lt;/ref&amp;gt; and he typically had little interest in lobbying the Indian government for funding to refine the design. In addition, however, elements of the IAF have been alleged to have held dismissive attitudes toward Tank and of his abilities, rarely coordinated with him on issues with the aircraft, which in turn exacerbated the type&amp;#039;s performance issues.&amp;lt;ref name = &amp;quot;smith 162&amp;quot;&amp;gt;Smith 1994, p. 162.&amp;lt;/ref&amp;gt; The level of technological transfer between Germany and India on the project was subject to criticism as well.&amp;lt;ref&amp;gt;Arnett 1997, pp. 119–120.&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Limitations within the Indian aerospace industry, which lacked the infrastructure and scientific base to successfully produce an effective indigenous combat aircraft at that time,&amp;lt;ref name = &amp;quot;Rajagopalan 116&amp;quot;/&amp;gt; forced a heavy reliance on foreign technologies and imported components.&amp;lt;ref name = &amp;quot;sat 480&amp;quot;/&amp;gt; HAL&amp;#039;s willingness to undertake overly-ambitious defence projects may also be partially responsible for the project&amp;#039;s outcome.&amp;lt;ref name = &amp;quot;sat 480&amp;quot;/&amp;gt; The Marut was not only heavily dependent on foreign-sourced materials, but was more expensive to manufacture the type in India than to have imported completed aircraft.&amp;lt;ref name = &amp;quot;gupta 34&amp;quot;/&amp;gt; The level of indigenous components increased over time, reportedly reaching 70 per cent by December 1973.&amp;lt;ref name = &amp;quot;times india 2016&amp;quot;/&amp;gt; The allocation of scarce resources to reproducing components that could have been readily imported represented a high level of [[opportunity cost]] to India.&amp;lt;ref name = &amp;quot;Rajagopalan 116&amp;quot;/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
The IAF reportedly showed little confidence or interest in indigenous fighter technology, having openly expressed its preference for the French-built [[Dassault Ouragan]] as an alternative.&amp;lt;ref name = &amp;quot;smith 162&amp;quot;/&amp;gt; By the time the Marut entered mass production, the IAF had already purchased foreign-built fighters such as the [[Hawker Hunter]] and [[Sukhoi Su-7]].&amp;lt;ref name = &amp;quot;arnett 120&amp;quot;&amp;gt;Arnett 1997, p. 120.&amp;lt;/ref&amp;gt; Following on from the Marut, HAL proceeded to produce larger quantities of both European and Soviet combat aircraft [[Licensed production|under license]], such as the [[SEPECAT Jaguar]], [[Mikoyan-Gurevich MiG-21]], and [[Mikoyan MiG-27]].&amp;lt;ref&amp;gt;Rajagopalan 2014, p. 138.&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Operational history==&lt;br /&gt;
[[File:HAL Marut used in the battle of longewala.jpg|thumb|A preserved Marut on static display. This aircraft had participated in the [[Battle of Longewala]].]]&lt;br /&gt;
&lt;br /&gt;
The Marut was used in combat in a ground attack role, where its safety features such as manual controls whenever the hydraulic systems failed, and twin engines, increased survivability. According to aviation author Pushpindar Singh, the Marut had excellent low-level flying characteristics, but its maneuverability suffered due to the lack of engine power; maintenance issues also resulted in the type being problematic in service.&amp;lt;ref name = &amp;quot;times india 2016&amp;quot;/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
In 1967, a single Marut was used as a testbed for the Egyptian indigenously-developed [[Brandner E-300]] engine.&amp;lt;ref name =&amp;quot;Janes 69 p671&amp;quot;&amp;gt;Taylor 1969, p. 671.&amp;lt;/ref&amp;gt; The Indian team was recalled in July 1969, while the Egypt-based Marut was abandoned.&amp;lt;ref name = &amp;quot;times india 2016&amp;quot;/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Given the limited number of Marut units, most Marut squadrons were considerably over-strength for the duration of their lives. According to Brian de Magray, at peak strength No.10 Squadron had on charge 32 Maruts, although the squadron probably did not hold a unit-establishment of more than 16. The Marut squadrons participated in the 1971 war and none were lost in air-to-air combat, although three were lost to ground fire, and one was destroyed on the ground. Three Marut pilots were awarded the [[Vir Chakra]] commendation.&amp;lt;ref&amp;gt;{{cite web |url=https://www.historynet.com/kurt-tanks-indian-storm.htm |title = Kurt Tank&amp;#039;s Indian Storm|date = 9 January 2022}}&amp;lt;/ref&amp;gt;&amp;lt;ref&amp;gt;{{Cite web|url=https://nationalinterest.org/blog/indias-disappointing-marut-jet-fighter-proved-itself-combat-21875|title=India&amp;#039;s Disappointing Marut Jet Fighter Proved Itself in Combat|date=13 August 2022}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Maruts constantly found themselves under heavy and concentrated fire from the ground during their low-level attack missions. On at least three occasions, Maruts regained their base after one engine had been lost to ground fire. On one of these, a Marut returned to base without escort on one engine, from about {{convert|150|mi|km|abbr=on}} inside hostile territory. On another occasion, a pilot flying his Marut through debris that erupted into the air as he strafed a convoy felt a heavy blow to the rear fuselage of the aircraft, the engine damage warning lights immediately illuminated, and one engine cut out. Fortunately, the Marut attained a safe and reasonable recovery speed on one engine. Consequently, the pilot had no difficulty in flying his crippled fighter back to base. Another safety factor was the automatic reversion to manual control in the event of a failure in the hydraulic flying control system, and there were several instances of Maruts being flown back from a sortie manually. The Marut had a good survivability record in enemy airspace.&amp;lt;ref&amp;gt;{{Citation | title = IAF | contribution = Marut | contribution-url = http://www.bharat-rakshak.com/IAF/History/Aircraft/Marut1.html | publisher = Bharat Rakshak}}.&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
In the [[Indo-Pakistani War of 1971]], some Maruts and [[Hawker Hunter]] aircraft were used to give close support to an Indian border post in the decisive [[Battle of Longewala]], on the morning of 5 December 1971. The aerial attack was credited with destroying a large number of tanks that had been deployed by Pakistani ground forces.&amp;lt;ref&amp;gt;Nordeen 2002, p. 81.&amp;lt;/ref&amp;gt; More than 300 combat sorties were flown by the Maruts during a two-week period in the war.&amp;lt;ref name = &amp;quot;times india 2016&amp;quot;/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
According to Indian reports, one aerial kill was recorded as having been achieved by a Marut. On 7 December 1971, Squadron Leader KK Bakshi of [[No. 220 Squadron IAF|No. 220 Squadron]] shot down a PAF F-86 Sabre (reportedly flown by Flying Officer Hamid Khwaja of [[No. 15 Squadron (Pakistan Air Force)|No. 15 Squadron]] of the [[Pakistan Air Force]]), however according to Pakistani reports, the [[F-86F]] Sabre (Serial No. 4030) had suffered an [[Engine flameout]] while chasing an Indian [[Hawker Hunter]] over Khushalgarh.&amp;lt;ref&amp;gt;{{Citation | title = IAF | contribution = Polly Marut | contribution-url = http://www.bharat-rakshak.com/IAF/History/Aircraft/Polly-Marut.html | publisher = Bharat Rakshak | access-date = 2014-08-25 | archive-date = 2008-01-28 | archive-url = https://web.archive.org/web/20080128190907/http://www.bharat-rakshak.com/IAF/History/Aircraft/Polly-Marut.html | url-status = dead }}&amp;lt;/ref&amp;gt;&amp;lt;ref&amp;gt;{{cite web&lt;br /&gt;
|url=http://www.pakdef.info/pakmilitary/airforce/1971war/paf_aircraft_losses.html&lt;br /&gt;
|title=PAF Aircraft losses (1971 War)&lt;br /&gt;
|date=&lt;br /&gt;
|publisher=PakDef.info&lt;br /&gt;
|access-date=2022-08-27&lt;br /&gt;
|archive-url=https://web.archive.org/web/20120712003410/http://www.pakdef.info/pakmilitary/airforce/1971war/paf_aircraft_losses.html&lt;br /&gt;
|archive-date=12 July 2022}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
[[File:HAL HF-24 Marut D-1205.jpg|thumb|right|HAL HF-24 D-1205 preserved at the Indian Air Force Museum , New Delhi.]]&lt;br /&gt;
&lt;br /&gt;
By 1982, the IAF was proposing that the Marut fleet be phased out on the basis that the type was &amp;quot;no longer operationally viable&amp;quot;.&amp;lt;ref name=&amp;quot;times india 2016&amp;quot; /&amp;gt; Supporters such as Air Commodore [[Jasjit Singh (IAF officer)|Jasjit Singh]] pointed out that the type had performed well in the 1971 combat, and had enjoyed superior safety records to other IAF aircraft such as the Gnat. Some aircraft had less than 100 recorded flight hours when the retirement of the Marut was being mooted.&amp;lt;ref name=&amp;quot;times india 2016&amp;quot; /&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Variants==&lt;br /&gt;
;HAL X-241:A full scale research glider replicating the proposed production aircraft, with identical dimensions, control configuration and aerofoil sections.&amp;lt;ref name=Bhargava/&amp;gt;&lt;br /&gt;
;Marut Mk.1: Single-seat ground-attack fighter.&lt;br /&gt;
;Marut Mk.1A: The third pre-production aircraft fitted with an afterburning [[Bristol Siddeley Orpheus 703]] with 18% boost at {{convert|5,720|lbf|kN|abbr=on|2}} thrust.&amp;lt;ref name=CHATTERJEE&amp;gt;{{cite web|last1=CHATTERJEE |first1=K. |title=HINDUSTAN FIGHTER HF-24 MARUT PART I: BUILDING INDIA&amp;#039;S JET FIGHTER |url=http://www.bharat-rakshak.com/IAF/History/Aircraft/Marut1.html |website=www.bharat-rakshak.com |access-date=10 June 2014 |url-status=dead |archive-url=https://web.archive.org/web/20130728144222/http://www.bharat-rakshak.com/IAF/History/Aircraft/Marut1.html |archive-date=28 July 2013 }}&amp;lt;/ref&amp;gt;&lt;br /&gt;
;Marut Mk.1 BX:A single Mk.1 converted as a flying test-bed for the [[Brandner E-300]] turbojet engine.&amp;lt;ref name=CHATTERJEE/&amp;gt;&lt;br /&gt;
;Marut Mk.1T: Two-seat training version.&amp;lt;ref name=CHATTERJEE/&amp;gt;&lt;br /&gt;
;Marut Mk.1R: Two HF-24s fitted with two afterburning [[Bristol Siddeley Orpheus 703]]s with 18% boost at {{convert|5,720|lbf|kN|abbr=on|2}} thrust.&amp;lt;ref name=CHATTERJEE/&amp;gt;&lt;br /&gt;
;Marut Mk.2:A projected [[Rolls-Royce Turbomeca Adour]] powered derivative.&amp;lt;ref name=CHATTERJEE/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Former operators==&lt;br /&gt;
; {{IND}}&lt;br /&gt;
* [[Indian Air Force]]&lt;br /&gt;
** [[No. 10 Squadron IAF]]&lt;br /&gt;
** [[No. 31 Squadron IAF]]&lt;br /&gt;
** [[No. 220 Squadron IAF]] – last unit with the type, relinquished aircraft mid-1990&amp;lt;ref&amp;gt;Bharat-Rakshak.com, [http://www.bharat-rakshak.com/IAF/History/Aircraft/Marut1.html HINDUSTAN FIGHTER HF-24 MARUT] {{webarchive|url=https://web.archive.org/web/20130728144222/http://www.bharat-rakshak.com/IAF/History/Aircraft/Marut1.html |date=2013-07-28 }}, accessed July 2009&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Surviving aircraft==&lt;br /&gt;
[[File:HAL-HF-24-Marut.jpg|thumb|HF-24 Marut preserved at the [[Deutsches Museum Flugwerft Schleissheim]] near Munich]]&lt;br /&gt;
&lt;br /&gt;
There are several surviving Maruts open to public inspection:&amp;lt;ref name=marutfabsnssubrid&amp;gt;{{cite web|title=Maruts on Display – Sublime to the Ridiculous|url=http://marutfans.wordpress.com/2010/09/20/maruts-on-display-sublime-to-the-ridiculous/|website=marutfans.wordpress.com|date=20 September 2010|access-date=10 June 2022}}&amp;lt;/ref&amp;gt;{{rs|date=March 2022}}&lt;br /&gt;
* [[Visvesvaraya Industrial and Technological Museum]], Bangalore.&lt;br /&gt;
* HAL Museum, Bangalore&lt;br /&gt;
* [[Kamala Nehru Park, Pune|Kamla Nehru Park]], Pune.&lt;br /&gt;
* Nehru Science Centre, [[Mumbai]].&lt;br /&gt;
* Periyar Science and Technology Centre, Chennai&lt;br /&gt;
* [[Aircraft &amp;amp; Systems Testing Establishment|ASTE]] (Aircraft &amp;amp; Systems Testing Establishment), Bangalore&lt;br /&gt;
* [[Air Force Academy, Dundigul]]&lt;br /&gt;
* [[Deutsches Museum Flugwerft Schleissheim]] now on display at [[Museum für Luftfahrt und Technik]] [[Wernigerode]]&lt;br /&gt;
* [[Indian Air Force Museum, Palam]]&lt;br /&gt;
&lt;br /&gt;
==Specifications (Marut Mk.1)==&lt;br /&gt;
[[File:Marut HF-24 trainer at HAL Museum 7652.JPG|thumb|Midsection of Marut. Note the two-seat cockpit and the placement of the air intakes]]&lt;br /&gt;
[[File:Marut HF-24 trainer at HAL Museum 7651.JPG|thumb|Closeup of a section of the underside of a Marut]]&lt;br /&gt;
{{Aircraft specs&lt;br /&gt;
|ref=Jane&amp;#039;s All The World&amp;#039;s Aircraft 1976–77 &amp;lt;ref name=&amp;quot;Janes 76 p79-80&amp;quot;&amp;gt;Taylor 1976, pp. 79–80.&amp;lt;/ref&amp;gt;&lt;br /&gt;
|prime units?=met&lt;br /&gt;
&amp;lt;!--&lt;br /&gt;
        General characteristics&lt;br /&gt;
--&amp;gt;&lt;br /&gt;
|genhide=&lt;br /&gt;
&lt;br /&gt;
|crew=1&lt;br /&gt;
|capacity=&lt;br /&gt;
|length m=15.87&lt;br /&gt;
|length ft=&lt;br /&gt;
|length in=&lt;br /&gt;
|span m=9.00&lt;br /&gt;
|span ft=&lt;br /&gt;
|span in=&lt;br /&gt;
|height m=3.60&lt;br /&gt;
|height ft=&lt;br /&gt;
|height in=&lt;br /&gt;
|wing area sqm=28.00&lt;br /&gt;
|wing area sqft=&lt;br /&gt;
|wing area note=&lt;br /&gt;
|aspect ratio=2.90:1&lt;br /&gt;
|airfoil=&lt;br /&gt;
|empty weight kg=6195&lt;br /&gt;
|empty weight lb=&lt;br /&gt;
|empty weight note=&lt;br /&gt;
|gross weight kg=&lt;br /&gt;
|gross weight lb=&lt;br /&gt;
|gross weight note=&lt;br /&gt;
|max takeoff weight kg=10,908&lt;br /&gt;
|fuel capacity={{convert|2491|L|USgal impgal|abbr=on}} usable internal fuel&lt;br /&gt;
|more general=&lt;br /&gt;
&amp;lt;!--&lt;br /&gt;
        Powerplant&lt;br /&gt;
--&amp;gt;&lt;br /&gt;
|eng1 number=2&lt;br /&gt;
|eng1 name=[[Bristol Siddeley Orpheus]] Mk 703&lt;br /&gt;
|eng1 type=[[turbojet]]s&lt;br /&gt;
|eng1 kn=21.6&amp;lt;!-- jet/rocket engines --&amp;gt;&lt;br /&gt;
|eng1 lbf=&amp;lt;!-- jet/rocket engines --&amp;gt;&lt;br /&gt;
|power original=&lt;br /&gt;
|thrust original=&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!--&lt;br /&gt;
        Performance&lt;br /&gt;
--&amp;gt;&lt;br /&gt;
|perfhide=&lt;br /&gt;
&lt;br /&gt;
|max speed kmh=1,112&lt;br /&gt;
|max speed note=at sea level&lt;br /&gt;
|max speed mach=0.93&lt;br /&gt;
|stall speed kmh=248&amp;lt;!-- if max speed unknown --&amp;gt;&lt;br /&gt;
|stall speed mph=&amp;lt;!-- if max speed unknown --&amp;gt;&lt;br /&gt;
|stall speed note=(flaps and landing gear down)&lt;br /&gt;
|never exceed speed kmh=&lt;br /&gt;
|never exceed speed mph=&lt;br /&gt;
|never exceed speed kts=&lt;br /&gt;
|range km=&lt;br /&gt;
|range miles=&lt;br /&gt;
|range nmi=&lt;br /&gt;
|combat range km=396&lt;br /&gt;
|combat range miles=&lt;br /&gt;
|combat range note=&amp;lt;ref name=&amp;quot;Donald World p523&amp;quot;/&amp;gt;&lt;br /&gt;
|endurance=&amp;lt;!-- if range unknown --&amp;gt;&lt;br /&gt;
|ceiling m=&lt;br /&gt;
|ceiling ft=&lt;br /&gt;
|g limits=&amp;lt;!-- aerobatic --&amp;gt;&lt;br /&gt;
|roll rate=&amp;lt;!-- aerobatic --&amp;gt;&lt;br /&gt;
|climb rate ms=22.5&lt;br /&gt;
|climb rate ftmin=4,444&lt;br /&gt;
|climb rate note={{fact|date=January 2022}}&lt;br /&gt;
|time to altitude=9 min 20 s to {{convert|40000|ft|m|disp=flip|abbr=on}}&lt;br /&gt;
|lift to drag=&lt;br /&gt;
|wing loading kg/m2=&lt;br /&gt;
|wing loading lb/sqft=&lt;br /&gt;
|wing loading note=&lt;br /&gt;
|more performance=&lt;br /&gt;
&amp;lt;!--&lt;br /&gt;
        Armament&lt;br /&gt;
--&amp;gt;&lt;br /&gt;
&lt;br /&gt;
|guns=4× 30 mm (1.18 in) [[ADEN cannon]] with 120 rpg&lt;br /&gt;
|rockets= Retractable [[Matra]] pack of 50× 2.68 in (68 mm) rockets&lt;br /&gt;
|bombs= Up to 4,000 lb (1,800 kg) on four wing pylons|missiles= &lt;br /&gt;
|hardpoints=&lt;br /&gt;
|hardpoint capacity=&lt;br /&gt;
|hardpoint rockets=&lt;br /&gt;
|hardpoint missiles=&lt;br /&gt;
|hardpoint bombs=&lt;br /&gt;
|hardpoint other=&lt;br /&gt;
&lt;br /&gt;
|avionics=&lt;br /&gt;
}}&lt;br /&gt;
&lt;br /&gt;
==See also==&lt;br /&gt;
{{External media|topic= |width=18% |align=right |video1=[https://www.youtube.com/watch?v=DcrymHmChK4 Video overview of the Marut] |video2=[https://www.youtube.com/watch?v=oxs4_SjtR1M News report on the 50th anniversary of the Marut&amp;#039;s first flight] |video3=[https://www.youtube.com/watch?v=sanS-K1dTRg Contemporary silent footage of the Marut at an air show, including an aerial display]}}&lt;br /&gt;
&lt;br /&gt;
{{Aircontent&lt;br /&gt;
|related=&lt;br /&gt;
|similar aircraft=&lt;br /&gt;
* [[Breguet 1100]]&lt;br /&gt;
* [[Fiat G.91Y]]&lt;br /&gt;
* [[Nanchang Q-5]]&lt;br /&gt;
* [[North American FJ-4 Fury]]&lt;br /&gt;
* [[Sukhoi Su-7]]&lt;br /&gt;
* [[Yakovlev Yak-26]]&lt;br /&gt;
|lists=&lt;br /&gt;
* [[List of aircraft of the Indian Air Force]]&lt;br /&gt;
* [[List of fighter aircraft]]&lt;br /&gt;
}}&lt;br /&gt;
&lt;br /&gt;
==References==&lt;br /&gt;
===Citations===&lt;br /&gt;
{{Reflist}}&lt;br /&gt;
&lt;br /&gt;
===Bibliography===&lt;br /&gt;
{{Refbegin}}&lt;br /&gt;
* Arnett, Eric H. &amp;#039;&amp;#039;Military Capacity and the Risk of War: China, India, Pakistan, and Iran&amp;#039;&amp;#039;. Oxford University Press, 1997. {{ISBN|0-19829-281-3}}.&lt;br /&gt;
* [http://www.flightglobal.com/pdfarchive/view/1964/1964%20-%201991.html &amp;quot;Maruta: India&amp;#039;s Hindustan HF-24 Joins the IAF&amp;quot;]. &amp;#039;&amp;#039;[[Flight International]]&amp;#039;&amp;#039;, 2 July 1964, Vol. 86, No. 2886. pp.&amp;amp;nbsp;16–17.&lt;br /&gt;
* Donald, David (editor). &amp;#039;&amp;#039;The Encyclopedia of World Aircraft&amp;#039;&amp;#039;. London:Aerospace, 1997. {{ISBN|1-85605-375-X}}.&lt;br /&gt;
* Gupta, Amit. &amp;#039;&amp;#039;Building an Arsenal: The Evolution of Regional Power Force Structures&amp;#039;&amp;#039;. Greenwood Publishing Group, 1997. {{ISBN|0-27595-787-X}}.&lt;br /&gt;
* Kumar, Satish. &amp;#039;&amp;#039;India&amp;#039;s National Security: Annual Review 2013&amp;#039;&amp;#039;. Routledge, 2015. {{ISBN|1-31732-461-7}}.&lt;br /&gt;
* Nordeen, Lon O. &amp;#039;&amp;#039;Air warfare in the missile age&amp;#039;&amp;#039;. Smithsonian Institution Press, 2002. {{ISBN|0-198-29168-X}}.&lt;br /&gt;
* Rajagopalan, Swarna. &amp;#039;&amp;#039;Security and South Asia: Ideas, Institutions and Initiatives&amp;#039;&amp;#039;. Routledge, 2014. {{ISBN|1-31780-948-3}}.&lt;br /&gt;
* Smith, Chris. &amp;#039;&amp;#039;India&amp;#039;s Ad Hoc Arsenal: Direction Or Drift in Defence Policy?&amp;#039;&amp;#039; Oxford University Press, 1994. {{ISBN|0-19829-168-X}}.&lt;br /&gt;
* [[John W. R. Taylor|Taylor, John W. R.]] &amp;#039;&amp;#039;Jane&amp;#039;s All The World&amp;#039;s Aircraft 1969–70&amp;#039;&amp;#039;. London:Jane&amp;#039;s Yearbooks, 1969.&lt;br /&gt;
* Taylor, John W.R. (editor). &amp;#039;&amp;#039;Jane&amp;#039;s All The World&amp;#039;s Aircraft 1976–77&amp;#039;&amp;#039;. London:Jane&amp;#039;s Yearbooks, 1976, {{ISBN|0-354-00538-3}}.&lt;br /&gt;
* Thomas, Raju G.C. &amp;#039;&amp;#039;Indian Security Policy&amp;#039;&amp;#039;. Princeton University Press, 2014. {{ISBN|1-40085-819-4}}.&lt;br /&gt;
{{Refend}}&lt;br /&gt;
&lt;br /&gt;
==External links==&lt;br /&gt;
{{Commons category}}&lt;br /&gt;
*[http://www.fas.org/man/dod-101/sys/ac/row/marut-1.jpg FAS page on HAL HF-24 Marut]&lt;br /&gt;
&lt;br /&gt;
{{HAL aircraft}}&lt;br /&gt;
{{Kurt Tank aircraft}}&lt;br /&gt;
&lt;br /&gt;
{{DEFAULTSORT:Hal Hf-24 Marut}}&lt;br /&gt;
[[Category:HAL aircraft|Marut]]&lt;br /&gt;
[[Category:1960s Indian fighter aircraft]]&lt;br /&gt;
[[Category:Twinjets]]&lt;br /&gt;
[[Category:Low-wing aircraft]]&lt;br /&gt;
[[Category:Aircraft first flown in 1961]]&lt;/div&gt;</summary>
		<author><name>Bot</name></author>
	</entry>
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