Proton (rocket family)

Soviet designed rocket family

Proton 8K82K

Launch of a Proton-K rocket carrying the Zvezda module to the ISS.

Function| Heavy-lift launch vehicle
Manufacturer|

* Khrunichev State Research and Production Space Center
* Chemical Automatics Design Bureau

Country of origin| Soviet Union * Russia
Size
Height| 53 m (174 ft)
Diameter| 7.4 m (24 ft)
Mass| 693,810 kg (1,529,590 lb), 3 stage
Stages|

* Proton-K: 3
* Proton-M: 4

Capacity
Payload to LEO
Mass| 23,700 kg (52,200 lb)[1]
Payload to GTO
Mass| 6,300 kg (13,900 lb)[1]
Launch history
Status| Active
Launch sites| Baikonur, LC-200 & LC-81
Total launches| 430

* Proton: 4
* Proton-K: 311
* Proton-M: 115

Success(es)| 382

* Proton: 3
* Proton-K: 275
* Proton-M: 104

Failure(s)| 44

* Proton: 1
* Proton-K: 34
* Proton-M: 9

Partial failure(s)| 4

* Proton-K: 2
* Proton-M: 2

First flight| Proton: 16 July 1965
Proton-K: 10 March 1967
Proton-M: 7 April 2001
Last flight| Proton: 6 July 1966
Proton-K: 30 March 2012
Proton-M: 12 March 2023
Carries passengers or cargo|

* Salyut 6
* Salyut 7
* Mir (all components except Docking Module)
* ISS components (Zarya, Zvezda, Nauka)
* ViaSat-1
* GLONASS
* ExoMars
* Spektr-RG
* Eutelsat 5 West B

First stage
Powered by| 6 × RD-275
Maximum thrust| 10,470 kN (2,350,000 lbf)
Burn time| 126 seconds
Propellant| N2O4/UDMH
Second stage
Powered by| 3 × RD-0210 & 1 × RD-0211
Maximum thrust| 2,399 kN (539,000 lbf)[2]
Specific impulse| 327 s (3.21 km/s)
Burn time| 208 seconds
Propellant| N2O4/UDMH
Third stage
Powered by| 1 × RD-0212
Maximum thrust| 630 kN (140,000 lbf)
Specific impulse| 325 s (3.19 km/s)
Burn time| 238 seconds
Propellant| N2O4/UDMH
Fourth stage – Blok-D/DM
Powered by| 1 × RD-58M
Maximum thrust| 83.4 kN (18,700 lbf)
Specific impulse| 349 s (3.42 km/s)
Burn time| 770 seconds
Propellant| LOX/RP-1

[edit on Wikidata]

Proton (Russian: Протон, formal designation: UR-500) is an expendable launch system used for both commercial and Russian government space launches. The first Proton rocket was launched in 1965. Modern versions of the launch system are still in use as of 2023[update], making it one of the most successful heavy boosters in the history of spaceflight. The components of all Protons are manufactured in the Khrunichev State Research and Production Space Center factory in Moscow and Chemical Automatics Design Bureau[3] in Voronezh, then transported to the Baikonur Cosmodrome, where they are assembled at Site 91 to form the launch vehicle.[4] Following payload integration, the rocket is then brought to the launch pad horizontally by rail, and raised into vertical position for launch.[5][6]

As with many Soviet rockets, the names of recurring payloads became associated with the launch vehicle itself. The moniker "Proton" originates from a series of similarly named scientific satellites, which were among the rocket's first payloads. During the Cold War, it was designated the D-1/D-1e or SL-12/SL-13 by Western intelligence agencies.

Launch capacity to low Earth orbit is about 22.8 tonnes (50,000 lb).[7] Geostationary transfer capacity is about 6.3 tonnes (14,000 lb).[8] Commercial launches are marketed by International Launch Services (ILS).[9]

In 2013, the rocket was intended to be retired before 2030.[10] As of June 2018[update], production on the Proton rocket is ceasing as the new Angara launch vehicle comes on line and becomes operational. No new launch service contracts for Proton are likely to be signed.[11]

## History

[edit]

Proton[12] started its life as a "super heavy ICBM". It was designed to launch a 100-megaton (or larger) thermonuclear weapon over a distance of 13,000 km. It was hugely oversized for an ICBM and was never deployed in such a capacity. It was eventually used as a space launch vehicle. It was the brainchild of Vladimir Chelomei's design bureau as a foil to Sergei Korolev's N1 rocket, whose purpose was to send a two-man Zond spacecraft around the Moon; Korolev openly opposed Proton and Chelomei's other designs for their use of toxic propellants.

The unusual appearance of the first stage results from the need to transport components by rail. The central oxidizer tank is the maximum width for the loading gauge of the track. The six tanks surrounding it carry fuel and serve as the attachment points for the engines. Despite resembling strap-on boosters, they are not designed to separate from the central oxidizer tank. The first and second stages are connected by a lattice structure. The second stage engine ignites shortly before separation of the first stage and the lattice allows the exhaust to escape.[13] This is called "hot staging" and it eliminates the need for ullage motors on the second stage.

A rushed development program led to dozens of failures between 1965 and 1972. Proton did not complete its State Trials until 1977, at which point it was judged to have a higher than 90% reliability.

Proton's design was kept secret until 1986, with the public being only shown the upper stages in film clips and photographs, and the first time the complete vehicle was shown to the outside world happened during the televised launch of Mir.

Mass-production of guidance, navigation and control system for Proton has begun in 1964 on "Communard" Industrial Association (Kharkov, Ukraine).[14]

Proton launched the uncrewed Soviet circumlunar flights and was intended to have launched the first crewed Soviet circumlunar spaceflights, before the United States flew the Apollo 8 mission. Proton launched the Salyut space stations, the Mir core segment and expansion modules, and both the Zarya and Zvezda modules of the ISS.

Proton also launches commercial satellites, most of them being managed by International Launch Services. The first ILS Proton launch was on 9 April 1996 with the launch of the SES Astra 1F communications satellite.[15]

Between 1994 and mid-2010, Proton revenues were $4.3 billion, and were projected to grow to $6 billion by 2011.[16]

In January 2017, the Proton was temporarily grounded due to the manufacturer, Voronezh Mechanical Plant, having substituted a heat-resistant alloy in the engines with a cheaper metal.[17][18]

In June 2018, the state corporation Roscosmos announced that the Proton rocket would cease production as the new Angara launch vehicle comes on line and becomes operational. No new launch service contracts for Proton are likely to be signed.[11]

Proton flew its last scheduled commercial mission on 9 October 2019, delivering Eutelsat 5 West B and Mission Extension Vehicle-1 to geostationary orbit.[19] A number of Roscosmos and other Russian government missions remain on Proton launch manifest.

## Proton K

[edit]

Main article: Proton-K

Proton K is fuelled by very toxic unsymmetrical dimethyl hydrazine and nitrogen tetroxide.[20] These are hypergolic fuels which ignite on contact, avoiding the need for an ignition system, and can be stored at ambient temperatures. This avoids the need for components that are tolerant of low temperatures, and allows the rocket to remain on the pad indefinitely (other launchers with such capability include the U.S. Titan II GLV, Titan III, and Titan IV, the Chinese Long March 2 and Long March 4, the Soviet/Ukrainian Tsyklon launchers, the Soviet/Russian Kosmos-3 and Kosmos-3M launchers and the European Ariane 1 to Ariane 4 launchers). In contrast, cryogenic fuels need periodic replenishment as they boil off.

The fourth stage has multiple variants, depending on the mission. The simplest, Blok D, was used for interplanetary missions. Blok D had no guidance module, depending on the probe to control flight. Three different Blok DM versions (DM, DM2, and DM-2M) were for high Earth orbits. The Blok D/DM were unusual in that the fuel was stored in a toroidal tank, around the engine and behind the oxidizer tank.

The initial Proton tests in 1965–66 only used the first two stages of the booster, the complete four-stage vehicle being flown for the first time in 1967. When the Soviet space station program began in 1971, Protons began being flown with the Blok D removed for use as a heavy-lift LEO launcher.

Proton-K payloads included all of the Soviet Union's Salyut space stations, almost all Mir modules (with the exception of the Docking Module, which was launched on the United States Space Shuttle), and the Zarya and Zvezda modules of the International Space Station. It was intended to launch the crewed TKS spacecraft, prior to the cancellation of that programme, although a few robotic flights of spacecraft were fulfilled. In addition it was intended to launch the 1970s LKS spaceplane that was never realised.[21]

The final launch of Proton-K was on 30 March 2012.

## Proton-M

[edit]

Main article: Proton-M

Proton-M, part being rotated to vertical. In the background, the mobile service tower can be observed.

The initial version of Proton M, could launch 3–3.2 tonnes (6,600–7,100 lb) into geostationary orbit or 5.5 tonnes (12,000 lb) into a geostationary transfer orbit. It could place up to 22 tonnes (49,000 lb) in low Earth orbit with a 51.6-degree inclination, the orbit of the International Space Station (ISS).

The Proton M's improvements included lower stage modifications to reduce structural mass, increase thrust, and fully use propellants. Generally a Briz-M (Russian: Бриз meaning Breeze) storable propellant upper stage is used instead of the Blok D or Blok DM stage, removing the need for multiple fuel supplies and oxygen top-off due to boiling; the Proton-M also flew with a Blok-DM upper stage. Efforts were also made to reduce dependency on foreign (usually Ukrainian) component suppliers. With the Briz-M upper stage, the payload fairing diameter is 4.1 m (13.45 ft).[22]

Proton launch vehicles and Briz-M upper stages are designed and built by Khrunichev State Research and Production Space Center (Khrunichev) in Moscow, the majority owner of International Launch Services (ILS). The center is home to all engineering, assembly and test functions of Proton production. With the recent consolidation of the Russian space enterprises, Khrunichev has direct oversight and control of up to 70% of all Proton manufacturing from suppliers to manufacturers. The consolidation directly supports Khrunichev's ongoing efforts for vertical integration of Proton production.[23]

### Phase III

[edit]

An enhanced variant, the Phase III Proton-M/Briz-M launch vehicle, was flight proven on the Russian Federal dual mission of Express AM-44 and Express MD-1 in February 2009 and performed its first commercial launch in March 2010 with the Echostar XIV satellite. The Proton-M/Briz-M phase III configuration provides 6150 kg of GTO performance, an increase of 1150 kg over the original Proton-M Briz-M, while maintaining the fundamental design configuration.

On 6 August 2012, the Russian Federal Space Agency lost a Russian and an Indonesian communications satellite in an attempt to launch them into orbit on a Proton-M due to technical difficulties with the last stage.[24]

On 2 July 2013, a Proton-M launching three GLONASS navigation satellites experienced a failure reminiscent of the 1960s disasters shortly after liftoff when the booster crashed near LC-39 at Baikonour, ending a 30-year unbroken stretch without a first stage failure; all future Proton flights were suspended pending investigation.[25] The accident was eventually determined to be caused by the rate gyro package having been installed upside-down. Due to the difficulty of installing the package incorrectly, it was widely suspected that it had been done deliberately by a disgruntled or drunk worker at the Khrunichev plant.[citation needed]

On 15 May 2014, a Proton-M/Briz-M carrying an Ekspress satellite suffered a third stage failure from a bad turbopump bearing. Debris fell in Manchuria. On 21 October, another Ekspress satellite was left in a useless orbit when the Briz stage cut off 24 seconds too early.

On 16 May 2015, a MEXSAT communications satellite failed to orbit due to another third stage malfunction, the eighth Proton failure since 2010.

### Phase IV

[edit]

Khrunichev has initiated development of a set of phase IV enhancements in order to keep pace with market demands and the mass growth trends of commercial satellites. The implementation of Phase IV Proton Briz-M enhancements were completed in 2016. The payload mass performance for phase IV has been increased to 6320 kg to a reference GTO orbit with 1500 m/s of residual delta V to GSO.[26]

## Future developments

[edit]

Significant upgrades were temporarily put on hold following announcement (in 1992) of the new Angara launch vehicle. The single largest upgrade [when?] was the KVRB stage. This cryogenic stage would have greatly increased capacity. The engine[which?] was developed successfully,[when?] and the stage as a whole had progressed to hardware. However, as KVRB is noticeably larger than Block D, the vehicle's aerodynamics, flight control, software, and possibly electronics would have to be reevaluated. In addition, the launch pad can supply existing Protons with common hypergolic fuels from single sources. The upper stages, in particular, are fed by common loading pipes running along the rocket. Switching to a stage with different fuels requires the addition of extra support articles; switching to cryogens requires that such support articles top off the stage periodically.[citation needed]

Heavy variants of Angara will be simpler and cheaper than Proton (and like the Atlas V rocket, will not use hypergolic fuels; instead, it will be a kerolox rocket, like the Soyuz rocket). They will also be designed from the start to accept a KVTK stage, and will already have a liquid oxygen supply at the pad; only a hydrogen supply will be called upon.[citation needed]

## See also

[edit]

* List of Proton launches
* Comparison of orbital launchers families
* Comparison of orbital launch systems

### Similar launch systems

[edit]

* Delta IV Heavy – Retired expendable launch system in the Delta rocket family
* Atlas V Heavy – Expendable launch system
* Ariane 5 – European heavy-lift space launch vehicle (1996–2023)
* Long March 5 – Chinese heavy lift rocket
* Angara A5 – Russian family of space launch vehiclesPages displaying short descriptions of redirect targets
* Falcon 9 – Orbital launch vehicle by SpaceX
* H-IIB – Expendable launch system
* Saturn I – American rocket used by space program
* Saturn IB – American rocket used in the Apollo program during the 1960s and 70s
* Heavy-lift launch vehicle – Launch vehicle capable of lifting over 20,000 kg into low Earth orbit

## References

[edit]

1. ^ a b Khrunichev State Research and Production Space Center - Proton-M rocket // russianforces.org
2. ^ "Proton 8K82K". www.friends-partners.org. Archived from the original on 16 November 2021. Retrieved 16 November 2021.
3. ^ АО "Конструкторское Бюро Химавтоматики" [JSC "Chemical Automation Design Bureau" (Khrunichev State Research and Production Space Center Homepage)].
4. ^ "Site 92 in Baikonur Cosmodrome". russianspaceweb.com. Retrieved 26 September 2022.
5. ^ "Proton Mission Planner's Guide". International Launch Services.
6. ^ "Proton Verticalization, Pad 39, Baikonur". flickr. 5 September 2005.
7. ^ Служебный модуль «Звезда» ['Zvezda' Service Module]. Khrunichev State Research and Production Space Center. Archived from the original on 16 April 2011.
8. ^ Clark, Stephen (9 June 2016). "Upgraded Proton booster adds satellite to Intelsat's fleet". Spaceflightnow.com.
9. ^ "Commercial Launch Heritage". International Launch Services.
10. ^ "Russian rocket development in the 2010s". Anatoly Zak.
11. ^ a b Berger, Eric (25 June 2018). "Russia's Proton rocket, which predates Apollo, will finally stop flying Technical problems, rise of SpaceX are contributing factors". arsTechica. Retrieved 26 June 2018. "...failures have followed in recent years. These problems, combined with the rapid rise of low-cost alternatives such as SpaceX's Falcon 9 rocket, have caused the number of Proton launches in a given year to dwindle from eight or so to just one or two."
12. ^ "Proton Heritage". International Launch Services.
13. ^ The first stage of the Proton rocket at Russian Space Web
14. ^ "History of SSIA "Communard"". Archived from the original on 27 January 2021. Retrieved 5 May 2019.
15. ^ "Proton Launch Archives | International Launch Services". ilslaunch.com. Retrieved 13 September 2014.
16. ^ "Statement by Vladimir Ye. Nesterov, Khrunichev Director-General, at Press Conference on 15 July 2010". Archived from the original on 24 September 2019.
17. ^ "Russia's Proton rocket grounded by poor quality control". www.planetary.org. Retrieved 26 January 2017.
18. ^ "Russia's Proton Rocket faces extended Grounding due to systemic Engine Problems". spaceflight101.com. 25 January 2017. Retrieved 24 February 2017.
19. ^ "Proton flies its last scheduled commercial mission". russianspaceweb.com.
20. ^ "Commercial Launch Vehicle | ILS Proton Breeze M | International Launch Services". ilslaunch.com. Retrieved 13 September 2014.
21. ^ Hendrickx, Bart; Vis, Bert (2007). "Beyond Buran - Chelomey's LKS". Energiya-Buran: The Soviet Space Shuttle. Space Exploration. Springer-Praxis. pp. 431–433\. doi:10.1007/978-0-387-73984-7. ISBN 978-0-387-69848-9.431-433&rft.pub=Springer-Praxis&rft.date=2007&rft_id=info:doi/10.1007/978-0-387-73984-7&rft.isbn=978-0-387-69848-9&rft.aulast=Hendrickx&rft.aufirst=Bart&rft.au=Vis,+Bert&rft_id=https://link.springer.com/book/10.1007/978-0-387-73984-7&rfr_id=info:sid/en.wikipedia.org:Proton+(rocket+family)" class="Z3988">
22. ^ "Proton Breeze M – ILS". www.ilslaunch.com. Retrieved 9 November 2019.
23. ^ "Experience ILS: Achieve Your Mission" (PDF). 4 March 2011. Archived from the original (PDF) on 17 January 2012.
24. ^ "News from around the world". latimesblogs.latimes.com. 7 August 2012. Retrieved 13 September 2014.
25. ^ "Russia's Proton crashes with a trio of navigation satellites". Russian Space Web. 2 July 2013.
26. ^ "Commercial Launch Heritage | Proton Rocket | International Launch Services". ilslaunch.com. Retrieved 13 September 2014.

## External links

[edit]

Wikimedia Commons has media related to:
Proton (Rocket) (category)

* Proton launches page on LyngSat
* Proton rocket specifications sheet
* Proton M Debuts With Successful Ekran Launch on April 7, 2001[usurped]
* Proton 8K82K / Briz-M. Astronautix.
* FAS – Proton Launch Vehicle Archived 2 June 2016 at the Wayback Machine
* ILS Proton
* Proton launch schedules on Satlaunch Archived 8 February 2021 at the Wayback Machine
* Слабое звено – "Бриз-М"

* v
* t
* e

Universal Rocket family

Variants|

| Main series|

* UR-100
* UR-200
* UR-500
* UR-700
* UR-900

|

UR-100 family|

* UR-100
* UR-100N
* Rokot
* Strela

UR-500 family|

* UR-500
* Proton
* Proton-K
* Proton-M
* Proton Medium
* Proton Light

Launch sites|

| Baikonur|

* Site 81
* Site 175
* Site 200

|

Plesetsk|

* Site 133

Launches|

* List of Proton launches
* 1965–1969
* 1970–1979
* 1980–1989
* 1990–1999
* 2000–2009
* 2010–2019
* 2020–2029

* See also: MR-UR-100

* v
* t
* e

Soviet and Russian 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
* Falcon 9 Block 5
* Falcon Heavy
* Firefly Alpha
* Gravity-1
* GSLV
* H-IIA
* H3
* 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
* 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
* SSLV
* Starship
* Tianlong-2
* Unha
* Vega
* C
* Vulcan Centaur
* Zhuque
* 2

In development|

* Antares 330
* Bloostar
* Blue Whale 1
* Cyclone-4M
* Deca
* Epsilon S
* Eris
* Gravity-2
* HANBIT-NANO
* Hyperbola-2
* Irtysh
* KSLV-III
* Kuaizhou
* 21
* 31
* Long March
* 9
* 10
* Miura 5
* MLV
* Neutron
* New Line 1
* NGLV
* Nova
* OS-M
* 2
* 4
* Orbex Prime
* Pallas-1
* Red Dwarf
* SLS
* Block 1B
* Block 2
* Soyuz-7
* Spectrum
* Terran R
* Tianlong-3
* VLM
* Vega E
* Zero
* Zhuque
* 3
* 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-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†

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

Soviet crewed lunar programs

Launch vehicles and
ascent/upper stages|

* N1 rocket
* Proton rocket
* Blok E
* Blok D

Spacecraft|

* LK-1
* VA spacecraft
* LK-700
* Zond (Soyuz 7K-L1)
* Zond-M (Soyuz 7K-L1S)
* Zond-LOK (Soyuz 7K-L1E)
* LOK (Soyuz 7K-L3)
* LK (spacecraft)

Other hardware|

* Lunokhod-LK
* Krechet-94

Soyuz docking tests|

* Soyuz 1, Soyuz 2A
* Soyuz 2, Soyuz 3
* Soyuz 4, Soyuz 5
* Soyuz 6, Soyuz 7, Soyuz 8
* Soyuz Kontakt 1, 2

Zond (7K-L1/L1S)
lunar flyby missions|

* Kosmos 146
* Kosmos 154†
* Zond 1967A†
* Zond 1967B†
* Zond 4
* Zond 1968A†
* Zond 1968B†
* Zond 5
* Zond 6
* Zond 1969A†
* Zond-M 1 (L1S-1)
* Zond-M 2 (L1S-2)†
* Zond 7
* Zond 8
* Zond 9
* Zond 10

* Kosmos 382

LOK (7K-LOK/L1E) test missions|

* Zond-LOK 1†
* LOK 1†
* LOK 2

LK Lander (T2K) test missions|

* Kosmos 379
* Kosmos 398
* Kosmos 434
* LK-1

The † sign designates failed missions. Italics designates cancelled missions.
*[v]: View this template
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*[e]: Edit this template