Rocket engine developed by Iran
Salman upper-stage Manufacturer IRGCASF Country of origin Iran Used on Qased
Qaem-100 Diameter 1 m (3 ft 3 in) Gross mass 1,900 kg (4,200 lb) Comparable Star 48 , Castor 30 Status Active Total launches 5 Successes (stage only) 5 Failed 0 First flight 22 April 2020
Burn time 60 seconds Propellant Solid
The Salman (Persian : سلمان ) is a solid-propellant rocket motor designed and built by the Islamic Revolutionary Guard Corps .[ 1] [ 2] It is used as the second stage of the Qased and Qaem-100 satellite launch vehicles .[ 1] [ 3] The system was announced on 9 February 2020[ 4] and was launched for the first time on 22 April 2020, placing Iran 's first military satellite, named Noor , into orbit.[ 1] [ 5]
Salman weighs 1,900 kilograms, has a diameter of 1 meter, and fires for 60 seconds. In contrast to previous Iranian commercial and military rocket designs, Salman has a wound carbon-fiber composite casing rather than the traditional steel motor casings typical of other Iranian designs, this drastically reduces weight and improves performance, allowing for more payload capacity.
Another break with past Iranian designs is the first ever use of gimballed thrust vector control (TVC) for steering as opposed to aerodynamic control surfaces , jet vanes , or vernier thrusters previously used.[ 5] [ 6] [ 7] A steerable nozzle provides several advantages to Salman as opposed to other methods that result in its superior performance and efficiency; as opposed to jet vanes , no thrust is lost in a gimballed system when steering; control surfaces only work in endo-atmospheric flight and cannot be used for injecting satellites or atmospheric re-entry ; vernier thrusters and their associated piping, turbopumps and tanks are heavy and their omission could make way for a larger payload.[ 8]
^ a b c Sheldon, John (12 May 2020). "#SpaceWatchGL Perspectives On Iran's Satellite Launch: Fabian Hinz On The Qased Satellite Launch Vehicle" . SpaceWatch.Global . Archived from the original on 29 March 2023. Retrieved 2 July 2021 .
^ "رفع گلوگاه پرتاب ماهواره با موتورهای فضایی سوخت جامد" [Elimination of Satellite Launch Bottlenecks with Solid-Fuel Space Engines]. ایرنا (in Persian). Islamic Republic News Agency . 15 May 2022. Archived from the original on 20 June 2022. Retrieved 18 November 2022 .
^ "سردار جعفرآبادی در گفتگو با العالم: قائم 100، ماهواره با وزن 80 کیلو را قادر است در مدار قرار دهد/ تداوم توسعه ماهوارهبر قائم تا قرارگیری ماهواره با وزن 500 کیلو در مدار/ قادریم ماهوارههای بزرگتری به مدارهای بالاتر حمل کنیم" [Sardar Jafarabadi in an interview with Al-Alam: Qaem 100 satellite, weighing 80 kilograms, is capable of being placed in orbit / Continuation of the development of the Qaem satellite launcher until a 500-kilogram satellite is placed in orbit / We are capable of transporting larger satellites to higher orbits.]. fa.alalam.ir (in Persian). 5 November 2022. Archived from the original on 23 May 2023. Retrieved 18 November 2022 .
^ "Iran unveils ballistic missile, 'new generation' engines" . The Times of Israel . 9 February 2020. Archived from the original on 10 July 2021. Retrieved 2 July 2021 – via Agence France-Presse .
^ a b Brügge, Norbert (25 August 2020). "What are the dimensions of the new Iranian Salman TVC solid-fuel rocket motor" . b14643.de . Archived from the original on 4 December 2022. Retrieved 2 July 2021 .
^ Hinz, Fabian (14 February 2020). "Iran's solid-propellant SLV program is alive and kicking" . armscontrolwonk.com . Archived from the original on 9 July 2023. Retrieved 2 July 2021 .
^ Elleman, Michael; Rouhi, Mahsa (1 May 2020). "The IRGC gets into the space-launch business" . International Institute for Strategic Studies . Archived from the original on 2 June 2023. Retrieved 2 July 2021 .
^ "گزارش تسنیم از موتور فضایی "سلمان"|درگیری با اهداف مهاجم خارج از جو زمین/ گام مهم سپاه برای ساخت سلاح ضدماهواره جاسوسی- اخبار نظامی | دف - اخبار سیاسی تسنیم | Tasnim" [Tasnim Report on the "Salman" Space Engine | Engagement with Invading Targets Outside Earth's Atmosphere / Important Step by the Revolutionary Guard in Building Anti-Spy Satellite Weapons]. خبرگزاری تسنیم | Tasnim (in Persian). 19 February 2020. Archived from the original on 3 October 2022. Retrieved 2 July 2021 .
^ "Iran launches its first military satellite" . Al Jazeera . 22 April 2020. Archived from the original on 25 May 2023. Retrieved 2 July 2021 .
^ "Iran test launches new satellite-carrying rocket" . Al Jazeera . 5 November 2022. Archived from the original on 26 May 2023. Retrieved 15 September 2023 .
^ Krzyzaniak, John [@john_krzyzaniak] (12 July 2023). "Here is the letter from Israel's representative to the UN, referenced above. On March 4, the IRGC launched a Ghaem-100 from Shahrud carrying the Nahid satellite" (Tweet ). Archived from the original on 30 August 2023. Retrieved 15 September 2023 – via Twitter .
^ "Iran says it launched Noor 3 satellite into orbit" . Reuters . 2023-09-27. Retrieved 2023-09-27 .
Iranian space program
Organizations Space centres Satellites
Reconnaissance/Spy Remote sensing Communication
Launch vehicles Spacecraft and capsules Astronomical observatories Primary spaceports People
Liquid fuel
Cryogenic
Hydrolox (LH2 / LOX )
China
Europe
India
Japan
Russia
United States
Methalox (CH4 / LOX )
China
United States
Russia
Europe
Semi- cryogenic
Kerolox (RP-1 / LOX )
China
India
Russia
NK-15
NK-33, 44
RD-58
RD-0105, 0109
RD-0107, 0108, 0110
RD-0110R
RD-0124
RD-107, 108, 117, 118
RD-120
RD-170, 171
RD-180
RD-191, 151, 181
RD-193
S1.5400
Spain
Ukraine
United States
Storable
Hypergolic (Aerozine , UH 25 , MMH , or UDMH / N2 O4 , MON , or HNO3 )
China
Europe
India
Israel
North Korea
Russia
17D61
RD-0202 to 0206, 0208 to 0213
RD-0207, 0214
RD-0216, 0217, 0235
RD-0233, 0234
RD-0236
RD-0237
RD-0243 to 0245
RD-0255 to 0257
RD-215 to 219
RD-250 to 252, 261, 262
RD-253, 275
RD-263, 268, 273
RD-270
S5.92
S5.98M
Ukraine
United States
Other
Solid fuel
China
Europe
India
Iran
Israel
Japan
United States
* Different versions of the engine use different propellant combinations
Engines in italics are under development