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Angara A5

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Russian heavy-lift launch vehicle

Angara A5
Size
Launch of the Angara-A5 from the Plesetsk cosmodrome on 19 June 2025
Function	Heavy-lift launch vehicle
Manufacturer	Khrunichev · KBKhA
Country of origin	Russia
Cost per launch	US$100 million (2021)^[1]
Height	55.4 m (182 ft)
Width	8.86 m (29.1 ft)
Mass	171,500–790,000 kg (378,100–1,741,700 lb)
Stages	2-3
Capacity
Payload toLEO (Plesetsk)
Mass	24,500 kg (54,000 lb)
Payload toGTO (Plesetsk)
Mass	5,400 kg (11,900 lb) - 7,500 kg (16,500 lb)

Associated rockets
Family	Angara
Comparable	Naro-1
Launch history
Status	Active
Launch sites	Plesetsk,Site 35 Vostochny,Site 1A
Total launches	5
Success(es)	4
Partial failure	1
First flight	23 December 2014
Last flight	19 June 2025(most recent)

Boosters –URM-1
No. boosters	4
Powered by	1 ×RD-191
Maximum thrust	1,920 kN (430,000 lb_f)
Total thrust	7,680 kN (1,730,000 lb_f)
Specific impulse	310.7 s (3.047 km/s)
Burn time	214 seconds
Propellant	LOX /RP-1
First stage –URM-1
Powered by	1 ×RD-191
Maximum thrust	1,920 kN (430,000 lb_f)
Specific impulse	310.7 s (3.047 km/s)
Burn time	325 seconds
Propellant	LOX /RP-1
Second stage –URM-2
Powered by	1 ×RD-0124A
Maximum thrust	294.3 kN (66,200 lb_f)
Specific impulse	359 s (3.52 km/s)
Burn time	424 seconds
Propellant	LOX /RP-1
Third stage –Briz-M (optional)
Powered by	1 ×S5.98M
Maximum thrust	19.6 kN (4,400 lb_f)
Specific impulse	326 s (3.20 km/s)
Burn time	3,000 seconds
Propellant	N₂O₄ /UDMH
Third stage –Blok DM-03 (optional)
Powered by	1 ×RD-58MF
Maximum thrust	19.6 kN (4,400 lb_f)
Specific impulse	326 s (3.20 km/s)
Burn time	3,000 seconds
Propellant	LOX /RP-1
Third stage –KVTK (optional, under development)
Powered by	1 ×RD-0146D
Maximum thrust	68.6 kN (15,400 lb_f)
Specific impulse	463 s (4.54 km/s)
Burn time	1,350 seconds
Propellant	LOX /LH₂

[edit on Wikidata]

Angara A5 (Russian:Ангара-А5), is a Russianexpendable heavy lift launch vehicle which consists of one URM-1 core and four URM-1 boosters, a 3.6-metre (12 ft) URM-2 second stage, and an upper stage, either theBriz-M,Blok DM-03 or theKVTK.^[2] Weighing 773 tonnes (1,704,000 lb) at lift-off, Angara A5 has a payload capacity of 24.5 tonnes (54,000 lb) to a 200 km (120 mi) x 60° orbit. Angara A5 is able to deliver 5.4 tonnes (12,000 lb) toGTO with Briz-M, or 7.5 tonnes (17,000 lb) to the same orbit with KVTK.^[2] Adding a kick stage increases the height of the rocket.

In the Angara A5, the four URM-1s used as boosters operate at full thrust for approximately 214 seconds, then separate. The URM-1 forming the vehicle's core is operated at full thrust for lift off, then throttled down to 30% to conserve propellant. The core is throttled back up after the boosters have separated and continues burning for another 110 seconds.^[3]

The first Angara A5 test flight was launched on 23 December 2014. The second test flight was launched on 14 December 2020 from Plesetsk.^[4]

Some official models show the Angara carrying anOrel crew capsulespacecraft with anabort tower.

Launch statistics

[edit]

Launch outcomes

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2014

2020

2022

'24

'25

'26

'27

Loss before launch
Loss during flight
Partial failure
Success
Planned

Launches

[edit]

Main article:"Angara" launch vehicles launches list

Date/time (UTC)	Configuration	Serial number	Launch pad	Outcome
	Payload	Separation orbit	Operator	Function
	Remarks
23 December 2014 05:57	Angara A5 /Briz-M	71751	Plesetsk,Site 35	Success
	IPM №1 (MGM №1)	LEO^[6]	RVSN RF	Mass simulator 2,000 kg (4,400 lb)
	Maiden flight of Angara A5, mass simulator intentionally not separated from Briz-M upper stage^[5] Orbital test flight No.1.
14 December 2020 05:50^[7]	Angara A5 /Briz-M	71752	Plesetsk,Site 35/1	Success
	IPM №2 (MGM №2)	GSO	RVSN RF	Mass simulator 2,400 kg (5,300 lb)
	Second orbital test flight. Orbital test flight No.2.
27 December 2021 19:00^[8]^[9]	Angara A5 /Persei	71753	Plesetsk,Site 35/1	Partial Failure
	IPN №1 (MGM №3)	Geocentric supersynchronous	RVSN RF	Mass simulator 5,400 kg (11,900 lb)
	First flight test of Blok DM-03 upper stage variant for Angara. Upper stage failed to restart for 2nd burn, leaving upper stage and payload in low Earth orbit. They decayed from orbit after about two weeks. Orbital test flight No.3.
11 April 2024 09:00	Angara A5 /Orion	72901	Vostochny,Site 1A	Success
	GMM-KA Gagarinets Dummy Cubesat	GEO LEO	Roscosmos	Mass simulator
	First flight test of the Angara A5 from Vostochny Cosmodrome (Vostochny Angara Test Flight). Orbital test flight No.4.
19 June 2025 03:00^[10]	Angara A5 /Briz-M	71754	Plesetsk,Site 35/1	Success
	Kosmos 2589 (14F166A №1) Kosmos 2590 (14F166A Subsat 1)	GEO	RVSN RF	Classified
	First operational launch of Angara A5. A new long fairing is used in this launch.
Future Launches
2025^[11]	Angara A5 /Briz-M		Plesetsk,Site 35/1
2025^[11]	Kosmos (14F166)	TBA	Russian Space Forces	TBA
Q4 2027^[12]^[13]	Angara A5M		Vostochny,Site 1A	TBD
	NEM-1	LEO/SSO	Roscosmos	Russian Orbital Service Station (ROSS) Core Module
	First flight of the Angara A5M. Originally intended for launch to the International Space Station. Now intended to go into a Sun-Synchronous Orbit at 98 degrees.
2028^[14]	Angara A5		Vostochny,Site 1A	TBD
	Orel	LEO	Roscosmos	Space capsule
	Uncrewed test launch of Orel spacecraft.
2028^[14]^[16]	Angara A5P		Vostochny,Site 1A	TBD
	Orel	LEO	Roscosmos	Space capsule
	Uncrewed test launch of Orel to the International Space Station. First flight of the Angara A5P, a crew-rated variant of the Angara A5.^[15]
2028^[14]^[15]	Angara A5P		Vostochny,Site 1A	TBD
	Orel	LEO	Roscosmos	Space capsule
	Crewed test launch of Orel to the International Space Station.
2028^[17]	Angara A5		Vostochny,Site 1A	TBD
	Luna 27	Selenocentric	Roscosmos	Lunar lander
	Third mission of Luna-Glob Programme.
NET 2029^[17]	Angara A5 /DM-03		Vostochny,Site 1A	TBD
	Luna 28	Selenocentric	Roscosmos	Lunar lander /Lunar sample return
	Lunar sample-return mission.
NET 2029^[16]	Angara A5P		Vostochny,Site 1A	TBD
	Orel	LEO	Roscosmos	Space capsule
	Crewed Orel flight test.
2030^[18]^[19]	Angara A5 /DM-03		Vostochny,Site 1A	TBD
2030^[18]^[19]	Spektr-UV	IGSO	Roscosmos	Ultraviolet space telescope
NET 2030^[17]	Angara A5		Vostochny,Site 1A	TBD
	Luna 29	Selenocentric	Roscosmos	Lunar rover /Lunar sample return
	Lunar sample-return mission.
NET 2030^[16]	Angara A5P		Vostochny,Site 1A	TBD
	Orel	LEO	Roscosmos	Space capsule
	Crewed Orel flight test.
NET 2030^[20]	Angara A5 /Briz-M		Vostochny,Site 1A	TBD
NET 2030^[20]	Spektr-M	Sun-Earth L2 Lagrange Point	Roscosmos	Millimeter wavelengthspace telescope

References

[edit]

^"MGM n°3". 24 December 2021. Retrieved24 December 2021.
^^a ^b"ГКНПЦ имени М.В.Хруничева | Семейство ракет-носителей "Ангара"". 2017-01-18. Archived fromthe original on 2017-01-18. Retrieved2023-11-26.
^"Angara A5 - Spaceflight101". 2015-09-25. Archived fromthe original on 2015-09-25. Retrieved2023-11-26.
^"Launch Schedule – Spaceflight Now". Retrieved2023-11-26.
^"Разгонный блок "Бриз-М" вывел на целевую орбиту условный спутник, запущенный на "Ангаре"" [Briz-M upper stage brought satellite to orbit, launched by Angara] (in Russian). ITAR-TASS. December 23, 2014. RetrievedDecember 23, 2014.
^"Russia made its first test launch "Angara-A5"". RIA Novosti. December 23, 2014. RetrievedDecember 23, 2014.
^Zak, Anatoly (3 October 2020)."Second mission of the Angara-5 rocket". RussianSpaceWeb.com. Retrieved14 December 2020.
^Mooney, Justin (27 December 2021)."Russia launches third and final Angara A5 demonstration mission".NASASpaceFlight. Retrieved30 December 2021.
^"Третий испытательный пуск тяжелой ракеты "Ангара-А5" осуществлен с космодрома Плесецк - Минобороны РФ" [The third test launch of the Angara-A5 heavy rocket was carried out from the Plesetsk cosmodrome - Russian Defense Ministry].Interfax (in Russian). 27 December 2021. Retrieved30 December 2021.
^Zak, Anatoly (2025-06-18)."Angara-5 carries its first payloads".RussianSpaceWeb.com. Retrieved2025-06-19.
^Zak, Anatoly (2025-03-12)."Space exploration in 2025".RussianSpaceWeb.com. Retrieved2025-03-13.
^"Russia to set up national orbital outpost in 2027 — Roscosmos".TASS. 24 January 2023. Retrieved31 January 2023.
^"Научно-энергетический модуль запустят на "Ангаре" с Восточного" [The Science Power Module will be launched on an Angara from Vostochny] (in Russian). Roscosmos. 24 April 2021. Retrieved28 April 2021.
^^a ^b ^cKatya Pavlushchenko [@katlinengrey] (15 August 2023)."Both the first uncrewed test flight and the first crewed test flight of the planned #Oryol spacecraft are scheduled for 2028, said the chief designer of ROS (it's not a misprint, now they call it ROS instead of ROSS), deputy director of RSC Energia Vladimir Kozhevnikov" (Tweet) – viaTwitter.
^^a ^b"Russia to create Angara-A5P rocket for manned space launches by 2024". TASS. 6 November 2019. Retrieved28 April 2021.
^^a ^b ^c"Определен срок полета российского корабля "Орел" с экипажем на МКС" [The scheduled time for the first crewed flight of the Russian spacecraft Orel to the ISS has been determined] (in Russian). RIA Novosti. 13 February 2020. Retrieved28 April 2021.
^^a ^b ^c"Ученый сообщил об активном ходе работ по импортозамещению комплектующих "Луны-27"" [The scientist reported on the active progress of work on import substitution of Luna-27 components].TASS (in Russian). 19 July 2023. Retrieved27 July 2023.
^"В Институте астрономии РАН заявили, что обсерваторию "Спектр-УФ" не запустят до 2030 года" [The Institute of Astronomy of the Russian Academy of Sciences said that the Spektr-UV observatory will not be launched until 2030].TASS (in Russian). 21 December 2023. Retrieved27 December 2023.
^Zak, Anatoly."Spektr-UF".RussianSpaceWeb. Retrieved5 February 2023.
^"Russia, France draft agreement on deep space exploration". TASS. 6 November 2019. Retrieved7 November 2019.

External links

[edit]

First "Angara A5" launch from "Vostochny" Cosmodrome

v t e Soviet andRussian launch vehicles
Active	Angara 1.2 A5 Soyuz-2 2.1a 2.1b UR Proton-M
In development	Amur Irtysh Yenisei
Retired	Dnepr Energia Kosmos 1 2I 3 3M N1 R-7 Luna Molniya M L Polyot Soyuz original L M U U2 FG 2.1v Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna Start-1 Tsyklon original 2 3 UR UR-500 Proton-K Rokot Strela Zenit 2 2M 3SL 3SLB 3F
Cancelled (no launch attempts)	Tsyklon-4 Proton Light Medium

v t e Orbital launch systems
List of orbital launch systems Comparison of orbital launch systems
Current	Angara 1.2 A5 Ariane 6 Atlas V Ceres 1 1S Chollima-1 Electron Eris^† Falcon 9 Block 5 Falcon Heavy Firefly Alpha Gravity-1 GSLV H3 HANBIT-NANO^† Hyperbola-1 Jielong 1 3 KAIROS^† Kaituozhe 2 Kinetica 1 Kuaizhou 1 1A 11 Long March 2C 2D 2F 3A 3B/E 3C 4B 4C 5 5B 6 6A 6C 7 7A 8 11 11H 12 12A LVM3 Minotaur I IV V C New Glenn Nuri OS-M1^† Pegasus XL Proton-M PSLV Qaem 100 Qased Shavit 2 Simorgh SLS Block 1 Soyuz-2 2.1a / STA 2.1b / STB Spectrum^† SSLV Starship Tianlong-2 Unha Vega C Vulcan Centaur Zhuque 2E 3
In development	Antares 330 Bloostar Blue Whale 1 Ceres-2 Cyclone-4M Deca Eclipse Epsilon S Gravity-2 Hyperbola-2 Irtysh Kinetica 2 2H 3 KSLV-III Kuaizhou 21 31 Long March 9 10 Miura 5 Neutron New Line 1 NGLV Nova OS-M 2 4 Orbex Prime Pallas-1 Red Dwarf RFA One SLS Block 1B Block 2 Soyuz-7 Terran R Tianlong-3 VLM Vega E Zero Zuljanah
Retired	Antares 110 120 130^† 230 230+ Ariane 1 2 3 4 5 ASLV Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able^† Agena Centaur Black Arrow Conestoga^† Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 II III IV IV Heavy Diamant Dnepr Energia Epsilon Europa I^† II^† Falcon 1 Falcon 9 v1.0 v1.1 v1.2 "Full Thrust" Feng Bao 1 GSLV Mk I H-I H-II H-IIA H-IIB Juno I Juno II Kaituozhe-1 Kosmos original 1 2/2I 3 3M Lambda 4S LauncherOne Long March 1 1D^† 2A 2E 3 3B 4A Mu 4S 3C 3H 3S 3SII V N1^† N-I N-II Naro-1 Paektusan^† Pilot-2^† R-7 Luna Molniya M L Polyot Soyuz original FG L M U U2 2-1v Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna^† Rocket 3 RS1^† Safir 1 1A 1B Saturn I IB V Scout X-1 Blue Scout II^† X-2^† X-2M X-3 X-3M X-4 X-2B^† B A B-1 D-1 A-1 E-1 F-1 G-1 Shavit original 1 SLV Space Shuttle SPARK^† Sparta SS-520 Start-1 Terran 1^† Thor Able Ablestar 1 2 Agena A B D Burner 1 2 Delta DSV-2U Thorad-Agena SLV-2G SLV-2H Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Tsyklon R-36-O original 2 3 Universal Rocket UR-500 Proton Proton-K Rokot Strela Vanguard Vega original VLS-1^† Zenit 2 2M 2FG 3SL 3SLB 3F Zhuque 1^† 2
Classes	Sounding rocket Small-lift launch vehicle Medium-lift launch vehicle Heavy-lift launch vehicle Super heavy-lift launch vehicle
This template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future Symbol^† indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)

v t e RD-170 rocket engine family
Derivatives	RD-171 RD-180 RD-191 RD-151
Technologies	Bipropellant LOX RP-1 Staged combustion cycle
Historic rockets	Atlas III (RD-180) Energia (RD-170) Naro-1 (RD-151) Zenit (RD-171)
Current rockets	Angara (RD-191) Antares (200-series) (RD-181) Atlas V (RD-180)
Cancelled proposals	GX (RD-180) Rus-M (RD-180)

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