Simorgh (, Simurgh), also called Safir-2, is an Iranian expendable launch vehicle. It is the successor of the Safir, Iran's first space launch vehicle. Its mission is to carry heavier satellites into higher orbit than Safir.

The project was unveiled by Iranian President Mahmoud Ahmadinejad on 3 February 2010, as part of celebrations of the first anniversary of the launch of Omid, the first indigenously launched Iranian satellite, and was launched for the first time on 19 April 2016.

Design Simorgh is a two-stage liquid-fueled rocket developed from the Safir rocket. It is able to place a payload into a circular low Earth orbit (LEO). It is also the first Iranian rocket that can place multiple payloads into orbit (e.g., one main payload and several secondary cubesats). In comparison, the Safir was only able to place a 50 kg payload into a 250x375 km elliptic orbit.

The Simorgh rocket is long, and has a launch mass of . Its first stage, with a diameter of 2.4 meters, is powered by a cluster of four synchronized Safir-1B first-stage engines with four separate turbopumps, each of these engines generating up to of thrust. The first stage also utilizes a set of four vernier engines sharing a single turbopump used for attitude control and providing an additional . At liftoff, these engines generate a total of thrust. The second stage with a diameter of 1.5 meters utilizes a set of four smaller engines similar to the two engines of Safir's second stage. These produce a total of thrust.

The Simorgh's total flight time to a 500-530km orbit is between 480 and 495 seconds. The first stage burns for about 102 seconds. Stages separation takes place at an altitude of 90 km and a velocity of 2300 m/s. The fairing shroud is ejected simultaneously with the second stage engine's ignition. The satellite is then accelerated to 7400 m/s and injected into its designated orbit.

In contrast to its predecessor Safir, the Simorgh is integrated and assembled vertically on a launch pad located at the Imam Khomeini Space Center. Each stage goes through manufacturing horizontally and is subsequently brought to the launch pad, where final assembly of the stages is completed with the aid of a custom-designed service tower.

Saman-1 is a solid-fueled orbital transfer system under development that produces of thrust and will be used as an additional upper stage in future.

Reliability The development of the Simorgh has been marked with difficulties and unreliability of certain sub-systems due to the overcomplexity of its engines and turbopumps. Out of the system's first four launches (two orbital and two sub-orbital launches) there have been three failures, giving the rocket a reliability rating of twenty five percent. There were however, indications of progressive improvements to the design and reliability of the system with each successive launch; with the 2017 launch operating for 120 seconds before failure, the 2019 launch operating 450 seconds before failure, and the 2020 launch operating correctly for 475 seconds out of the 490 seconds of operation required for a successful mission, giving the missions a 25, 92, 97, percent success rate respectively, indicating a trend of increasing reliability in the design.

Launch history Satellite(s) Date & Time (UTC)Launch site Satellite Mass Outcome Remarks No payload 19 April 2016Semnan LP-2N/A SuccessSub-orbital test flight. No payload 27 July 2017Semnan LP-2100 kg FailureOrbital test flight. Simorgh operated for 136 seconds. Second stage failed. Payam (named "AUT-SAT" previously) 15 January 2019Semnan LP-290 kg FailureOrbital test flight. Simorgh operated for 455 seconds. Third stage failed. Zafar-1https://spaceflightnow.com/2020/02/10/iran-fails-in-satellite-launch-attempt/ - 11 February 2020 9 February 2020, 15:45Semnan LP-2113 kg FailureOrbital test flight. Simorgh operated for 475 seconds. Satellite reached speed of 6,500 m/s out of the 7,400 m/s required to orbit. First stage operated fully correctly. Second stage failed. Unknown 12 June 2021Semnan LP-2 Disputed launch existenceU.S. official stated "is aware of an Iranian rocket launch failure". Satellite imagery "looked like a launch" occurred. Iran's Telecommunications Minister denied any launch. Three research devices 30 December 2021Semnan LP-2TBA FailureOrbital test flight.First time Iran launched multiple payloads in the same launch. Simorgh operated for about 600 seconds (500 seconds for the second stage). Devices didn't enter orbit; reached an altitude of 470 km and a speed of 7,350 m/s, out of the 7,600 m/s required.Mahda, Keyhan-2 and Hatef-128 January 2024Semnan LP-2TBA SuccessFirst successful orbital launch of Simorgh, placed three satellites into a 1100 x 450 km orbit. The launch occurred just 8 days after the first successful orbital launch of Qaem 100.Saman-1, Fakhr-1 and one other research satellite6 December 2024Semnan LP-2300 kg SuccessThe launch of the Saman-1 orbital transfer block to an altitude of 400 kilometers, along with two other payloads (including the Fakhr-1 satellite), with a total weight of 300 kilograms, breaking weight record.Navak-118 February 2025Semnan LP-240 kg FailureReports initially stated that Iran planned to launch the 40 kg "Navak" satellite into GTO orbit (200 to 31,000 km altitude) on February 18, 2024.

However, updates on the mission stopped, suggesting the launch may have failed — though officials likely withheld the news to avoid harming the country’s image.

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See also Comparison of orbital launchers families Comparison of orbital launch systems Iranian Space Agency Saman-1 (rocket stage) Other Iranian satellite launch vehicles Safir (rocket) Qased (rocket) Qaem-100 (rocket) Zuljanah (rocket)

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