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Related pages:

Light

Proton-Light


Proton-M

Proton-M


Crash

Proton crash with GLONASS satellites


RD-253

RD-253/275 engines


Operations

Proton launch facilities in Baikonur


M69

Mars-69 mission


 

Rollout

Above: A three-stage Proton rocket moves to its launch pad in Baikonur in July 2000. This version of the vehicle launched Soviet Salyut space stations, the core module of the Mir space station and the Zvezda service module for the International Space Station.

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No other launcher has played as many roles in the Russian space program as has the UR-500 rocket, known today as Proton. Conceived at the dawn of the space race as a "super-size" ICBM, the UR-500 became a major player in the race to the Moon in the mid-1960s. In the 1970s and 1980s, the four-stage version of the launch vehicle launched Soviet planetary probes toward the Moon, Mars, Venus and Halley Comet and allowed the Soviet Union to place satellites into geostationary orbit. At the same time, three-stage Protons launched all Soviet space stations, as well as heavy transport ships and modules to expand and resupply them in space. The rocket was formally declared operational only in 1978.

In the 1990s, the Proton became the workhorse of Russia's commercial launch business, winning its first contract to deliver an Inmarsat communications satellite in 1993 and launching its first commercial payload on April 9, 1996. After almost half a century in operation, Proton rockets logged 400 missions by the end of 2014. Around the same time, Briz-M space tug, serving as Proton's newest fourth stage, logged more than 70 missions. More than 450 satellites were launched during this period, according to the rocket's developer GKNPTs Khrunichev.

production

Proton's main production line in Moscow.

The third stage

After initial four test launches, Proton was upgraded with a third stage, which became a standard part of the vehicle. It is currently propelled by an RD-0212 multi-engine propulsion system, which includes the RD-0213 main engine and a four-chamber steering thruster known as RD-0214. Both propulsion units were developed at the KBKhA design bureau in the city of Voronezh and mass produced by an adjacent mechanical plant, VMZ.

Proton-M (Proton-KM)

The Proton-M, sometimes identified as Proton-KM, featured several modifications, which were designed to increase the payload and reliability of the vehicle, compared to the previous version of the rocket, known as Proton-K. For the first time, a digital flight control system replaced traditional analog hardware onboard Proton. It allowed more efficient propellant consumption during the flight and, as a result, the delivery of bigger payloads into orbit. The rocket became even more powerful thanks to a new version of the RD-253 engines on its first stage. Moscow's Energomash development center increased the thrust of the engine from 151 to 160 tons. With these two improvements the Proton-M was able to deliver 22 tons of cargo into low Earth orbit compared to 20.7 tons for the standard Proton-K booster.

Proton-M/Briz-M vehicle made its successful inaugural flight in 2001 and delivered its first commercial payload on Dec. 30, 2002.

Briz-M

For missions beyond initial low orbits, the new Proton was equipped with a more advanced fourth stage called Briz-M. The new stage completed its inaugural flight onboard a regular Proton-K booster in May 2000, when it is delivered the Gorizont communications satellite. Briz-M takes much less space onboard the launch vehicle compared to its predecessor, the Block D upper stage, leaving the freed volume for cargo. As a result, the new payload shroud topping the rocket could offer 2.5 times more room for the satellites onboard Proton-M.

Further modifications

For a number of years, Khrunichev enterprise in Moscow, which builds the Proton rocket, hoped to introduce even more drastic changes in the Proton's design. KB Salyut, Khrunichev's development arm, planned a much more powerful upper stage than the Briz-M. Designated KVRB, it was to employ super-cold liquid hydrogen and liquid oxygen -- the same propellant used in the US Space Shuttle's main engines and in the Energia rocket. The development of a cryogenic stage initiated by Khrunichev in 1980s was stalled for years by Russia's financial problems. Work, however, has progressed somewhat during the first decade of the 21st century, thanks to commercial deals with India, which eyed similar technology for its own space launcher. KB Salyut has developed the cryogenic upper stage for the Indian government and hopes to use its off-the-shelf technology for the even bigger stage for Proton. KB Salyut representatives said that the Proton's cryogenic stage would house 18 tons of propellants compared to the 12 tons carried by the stage developed for the Indian rocket. With the new cryogenic stage, Proton would be able to compete with the Ariane-5 rocket, the most advanced European launcher, despite the geographical disadvantage of flying from Kazakhstan compared to Ariane's launch pad in equatorial region of French Guiana.


Lockheed Martin ends its partnership with Khrunichev

On Sept. 7, 2006, the American aerospace giant Lockheed Martin announced the sale of its stake in the International Launch Services, ILS, which had been marketing the Russian Proton rocket to commercial clients around the world. The move ended a more than decade-long partnership between Lockheed Martin and the Moscow-based GKNPTs Khrunichev, the Proton manufacturer.


Proton modifications for 2011

In the first decade of the 21st century, developers planned a new series of upgrades to the Proton M rocket and its Briz-M upper stage to increase its payload to geostationary transfer orbits from 6,150 kilograms to 6,300 kilograms. Modifications to the Briz-M would enable it to fly so-called supersync missions, in which payloads are inserted into a supersynchronous orbit with an apogee of 65,000 kilometers or almost twice higher than the final altitude for a typical communications satellite. Such a trajectory on the way to a regular geostationary orbit would yield around 150-200 kilograms in extra payload mass. This is close to the payload capacity which was lost after Kazakhstan banned the launch path to the 48-degree parking orbit. The Kazakh government's decision to prohibit launches below the standard 51-degree parking orbit after 2009 was at least partially prompted by a JCSAT-11 launch failure, which resulted in debris crashing within 40-50 miles of the town of Dzhezkazgan. The first missions using supersync launch profile were scheduled for 2011, however not all satellites would be capable of supporting such flight sequences. As a result, Proton was expected to fly both types of missions.

In the meantime, the last Proton-K rocket launched on March 30, 2012, with the last Oko early warning satellite.


Proton-Light proposed

Looking to expand payload capabilities of the Proton rocket downwards, its developer proposed smaller, cheaper version of Russia's commercial space workhorse in 2016. If ever built, the Proton-Light variant is expected to have the industrial designation 8K82KL.


 

 

Different versions of UR-500 (Proton) rocket:

Type
Manufacturer index
US designation
Developer
Payloads
UR-500
8K82
SL-9
OKB-52
Proton 1-4, LK
UR-500K (Proton-K)
8K82K
SL-12/13
TsKBM
Salyut
UR-500K-L1 (UR-500K-L1P)
8K82K
SL-12
TsKBM
L1
UR-500KM (Proton-M)
8K82KM
-
KB Salyut
-
Proton-Light
8K82KL
-
GKNPTs Khrunichev (KB Salyut)
-

 

Proton development contractors:

Component
Developer Location
Overall design
OKB-52 (Branch 1)
Reutov
Production
Zavod Khrunicheva
Moscow (Fili)
Propulsion units (Stage I)
OKB-456
Moscow
Propulsion units (Stage II and Stage III)
KBKhA
Voronezh
Control system
NII-885
Moscow
Launch complex (surface)
Spetsmash
Moscow
Stage structures and mechanical components
PO Polyot
Omsk
Batteries for Proton-M
Hawker (EnerSys)
Zurich (Switzerland)
Inter-stage carbon structures, adapters
TsNII SM
Khot'kovo, Moscow Region

 

Early missions of the Proton rocket:

1965 July 16, 14:16 Moscow Time: The first Proton rocket (No. 207) lifts off from Site 81 in Tyuratam carrying the Proton-1 spacecraft. (355)

1965 Nov. 2: A Proton rocket lifts off from Site 81 in Tyuratam carrying the Proton-2 spacecraft.

1966 March 24: A Proton fails to deliver a spacecraft after launch from Site 81 in Tyuratam.

1966 July 6: A Proton rocket lifts off from Site 81 in Tyuratam successfully delivering the Proton-3 spacecraft.

1967 March 10: An UR-500K rocket equippped with a Block D upper stage lifts off from Site 81 in Tyuratam carrying the first prototype of the 7K-L1 circumlunar spacecraft. It was announced as Kosmos-146.

1967 April 8: A Proton rocket with a Block D upper stage lifts off from Site 81 in Tyuratam carrying a prototype of the 7K-L1 circumlunar spacecraft. It was announced as Kosmos-154.

1967 Sept. 28: A Proton rocket with a Block D upper stage fails to deliver a prototype of the 7K-L1 circumlunar spacecraft (Vehicle No. 4L). The launch was not announced.

1967 Nov. 22: A Proton rocket with a Block D upper stage fails to deliver a prototype of the 7K-L1circumlunar spacecraft after launch from the newly completed "right" launch pad (known today as Number 24) of Site 81 in Tyuratam. The launch was not announced.

1968 March 2: A Proton rocket with a Block D upper stage lifts off from the "left" launch pad at Site 81 in Tyuratam carrying a prototype of the L1 circumlunar spacecraft. It was announced as Zond-4.

1968 April 23: A Proton rocket with a Block D upper stage fails to deliver a prototype of the L1 circumlunar spacecraft after launch from the "right" launch pad at Site 81. The launch was not announced.

1968 July 14: An explosion at the Proton launch complex with a L1 (Zond) spacecraft in pre-launch processing kills one person.

1968 Sept. 15: A Proton rocket with a Block D upper stage lifts off from the "left" launch pad at Site 81 in Tyuratam carrying a prototype of the L1 circumlunar spacecraft. It was announced as Zond-5.

1968 Nov. 16: A Proton rocket successfully launches the Proton-4 science spacecraft from the "right" launch pad of Site 81 in Tyuratam.

1969 Jan. 20: A Proton rocket fails to place an L1 spacecraft into orbit after launch from "left" launch pad of Site 81 in Tyuratam.

1969 Feb. 19: A Proton rocket fails to place a lunar probe into orbit after launch from "right" launch pad of Site 81 in Tyuratam.

1969 March 27: A Proton rocket fails to place a Mars-69 spacecraft in orbit after launch from "right" pad at Site 81 in Tyuratam.


 

Recent Proton missions in detail and their statistics:

Year
Total missions
Failed launches
Success rate*
2001
6
0
-
2002
9
1
-
2003
5
0
-
2004
8
0
-
2005

7

0
-
2006
6
1
-
2007
7
1
-
2008
10
1
-
2009
10
0
-
2010
12
1
94.0 percent
2011
9
1
93.3 percent
2012
11
2
81.8 percent
2013
10
90.0 percent
2014
8
2
-
2015
8
-
2016
3
0
-
2017
In progress
0
-
-
129
12
90.6 percent

*Success rate for the reported period since 2001

 

In-depth overview of recent Proton missions:

Proton missions in 2013:

Proton missions in 2014:

Proton missions in 2015:

Proton missions in 2016:

Proton missions in 2017:

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Page author: Anatoly Zak; Last update: September 28, 2017

Page editor: Alain Chabot; Edit history: February 12, 2008; January 23, 2011

All rights reserved

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PICTURE GALLERY

L1

The Proton rocket with the L1 spacecraft for circumlunar missions is poised for launch in Baikonur.


L1

Proton lifts off with an L1 spacecraft. Credit: GKNPTs Khrunichev


The concept of the UR-500LKS complex, designed to carry the LKS "mini-shuttle" into orbit. Credit: NPO Mash


Proton

A three-stage Proton lifts off with a Soviet space station. Credit: GKNPTs Khrunichev


Proton

A four-stage version of the Proton rocket, likely photographed during the 1984 launch of the Vega spacecraft toward Venus. Credit: GKNPTs Khrunichev


1980s

A likely launch of the Proton rocket with an Almaz unmanned satellite at the end of the 1980s. Credit: GKNPTs Khrunichev


Kristall

A Proton rocket with the Kristall module of the Mir space station sits on the launch pad in Area 200 of Baikonur Cosmodrome, shortly before launch on May 31, 1990.


FGB

The Proton rocket with the Zarya FGB control module is being erected on the launch pad in November 1998. Click to enlarge.


FGB fairing

The payload fairing, which covered the FGB module during its ride to orbit onboard the Proton rocket in November 1998. Click to enlarge. Credit: Khrunichev


Yamal

A scale model of the head section of the Proton rocket with Block D upper stage and a pair of Yamal satellites. Click to enlarge. Copyright © 2009 Anatoly Zak


The scale model of the Proton-M rocket with the KVRB hydrogen-powered upper stage. Copyright © 2001 Anatoly Zak


Comparison of Proton-K and Proton-M launch vehicles. Credit: ILS


Tail view of the Proton rocket shows its first stage with six external tanks and six main RD-275 engines. Copyright © 2000 Anatoly Zak


The RD-301 engine intended for the Proton's 11S813 fourth stage, which would burn a mix of liquid fluorine and ammonia! The combination, which has been under development since July 1969, was designed for the delivery of the SNTV telecommunications satellite. The program of both the satellite and its upper stage was canceled in 1977. Copyright © 2002 Anatoly Zak