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US-A
Part of Kosmoplan
US-A
US-A
Credit: © Mark Wade
Russian military naval surveillance radar satellite. The US-A (later known as RLS) was a nuclear powered RORSAT (Radar Ocean Reconnaissance Satellite). Ocean surveillance, active radar satellite, Russia. Launched 1970 - 1988. Used US-Bus.

AKA: 17F16;17K114;US-AM. Status: Operational 1965. First Launch: 1965-12-27. Last Launch: 1988-03-14. Number: 38 . Gross mass: 4,300 kg (9,400 lb).

It used an active radar to track naval vessels from space in darkness and all weather.

The RLS was an element in the integrated Soviet weapons system devoted to destruction of the US Navy's surface and submarine forces. The system used space-based platforms to obtain the location of enemy forces at sea. This targeting information was provided to aircraft, surface vessels, and submarines and fed into anti-ship missiles that would attack the US forces from over the horizon. The US-A had a complex development history, with three chief designers overseeing its development. It was conceived and designed by Chelomei in 1959-1964; redesigned and flight tested by Savin in 1965-1969; and finally completed and put into service by KB Arsenal from 1969 on. The nuclear reactor aboard the US-A crashed to earth several times, causing international incidents. Furthermore the RLS had the lowest reliability and most quality problems of any Soviet space system. Nevertheless the system eventually allowed the Soviet Union to continuously monitor naval traffic throughout the oceans of the world.

The spacecraft was equipped with two side-looking radar antenna structures, guaranteeing the capability of locating naval targets in all weather, day or night, including those maintaining radio silence. The spacecraft bus provided 3 axis stabilization and the nuclear reactor was put in a safe graveyard orbit after completion of the mission. In the event of failure to place the reactor in the graveyard orbit, a backup system ejected the reactor core and dispersed the fuel during re-entry, spreading the radioactive material in the upper atmosphere so that a safe radiation exposure standard was reached. The multi-function engine section kept the spacecraft oriented during flight, maintained the orbital altitude, and deorbited the spacecraft at the end of the mission. The overall system was designated 17K114 (space complex for naval space reconnaissance and targeting purposes). The spacecraft had the article number 17F16.

Beginning in the late 1950's, Chelomei began studying use of his encapsulated cruise missile technology for spacecraft. A whole family of unmanned spacecraft, dubbed Kosmoplans, would be built using modular elements. One variant of the Kosmoplan would conduct naval radar and signals reconnaissance, launched by the UR-200 rocket.

In 1959, as Chelomei laid out these plans, he knew a tremendous struggle would be required to wrest a piece of the space program from Chief Designer Korolev. But Chelomei had stacked the deck against Korolev by hiring Khrushchev's son as a lead engineer at his OKB. By 30 May 1960 Korolev presented to the Soviet leadership a plan that now included participation of Chelomei. One project allocated to Chelomei was theme US - Upravlenniye Sputnik - a naval reconnaissance satellite using a P6 nuclear reactor for active tracking and targeting American warships. This was to be developed in 1962 to 1964. Chelomei was authorized by Decree 715-296 of 23 June 1960 'On the Production of Various Launch Vehicles, Satellites, Spacecraft for the Military Space Forces in 1960-1967' to complete a draft project on unpiloted Kosmoplans.

At the beginning of the 1960's the Soviet Union had developed anti-ship missiles of very long range but the problem of locating the missile's targets had not been solved. The first resolution for development of a Kosmoplan-derived Naval Space Reconnaissance and Targeting System (MKRTs) was issued in March 1961. The Kosmoplan's UR-200 (8K81) launch vehicle was approved for production on 16 March and 1 August 1961 by the Central Committee and Politburo. The Kosmoplan and UR-200 draft projects were completed in July 1962. Trial flights of the ICBM version of the UR-200 ran from 4 November 1963 to 20 October 1964.

Basic research on the concept was conducted by several rocket, radio-technical, and electro-technical design bureaus and research institutes. These included work done by FEI and the Kurchatov Nuclear Research Institute on a compact reactor to power the satellite. Theoretical research in the optimum orbit for the system was undertaken at the Academy of Sciences under Keldysh. The spacecraft was developed by Chelomei at OKB-52 and A A Raspletin at KB-1 MRP. M M Bondaryuk, G M Gryaznov, and V I Serbin at OKB-670 developed a thermal analogue of the nuclear power plant.

On October 13, 1964, Khrushchev was ousted from power. The new leadership, under Brezhnev, was adverse to all projects Khrushchev had supported, particularly those of Chelomei. An expert commission under M V Keldysh decided to cancel the UR-200, while the US was assigned to KB-1. Manager for the system at KB-1 was A I Savin, who was head of the renamed TsNII Kometa after 1973. The spacecraft was to be redesigned for launch by the Tsyklon 2 version of Yangel's R-36 rocket.

Two separate versions of the spacecraft were to be developed. The reactor-powered US-A would use active radar to track naval vessels in any weather. The solar-powered US-P would provide SIGINT services for the Soviet Navy and track naval ships passively. The spacecraft was still by TsKBM MOM (Chelomei) and the US-A's radar by NPO Vega GKRE. The project was jointly managed by the VMF Soviet Navy's Directorate for Rocket-Artillery Forces (URAV) and the GUKOS Military Space Force.

By the end of the 1960's development was largely complete, including flight tests from 1965 of mass models and experimental prototypes equipped with orientation, stabilization, and radio-control systems. But the principal radar system had not completed development and was not available for flight test. Finally it was decided that Chelomei's NPO Mash just didn't have the resources to bring the project to completion. Furthermore the design bureau had additional tasks with development of the Almaz and DOS space stations. Therefore Afanasyev decided to transfer the entire project to NPO Arsenal in May 1969. Arsenal had proven itself in development of the RT-2, RT-15, and D-II solid propellant ballistic missiles and had extensive test stands available that could be used for spacecraft development.

Work on spacecraft at KB Arsenal began in 1969 with the turnover to Arsenal of the documentation on these Chelomei-designed unmanned spacecraft. Arsenal was made responsible for series production and development of new variants. V F Kalabin was named head of the new space section.

MKRTs still consisted of two satellites. The RLS (ex-US-A) satellite would be equipped with an RLS radar location system powered by a YaEU nuclear reactor. The documentation handed over to Arsenal on the RLS was nearly complete and Chelomei's NPO Mash was pressured to complete the RLS drawings and release them to the factory.

Ye K Ivanov was Chief of the Design Bureau and Director of the Factory at KB Arsenal. Head project engineers for MKRTs were N N Kazakov and I A Abramov. The following were the principal subcontractors:

This was a new area for Arsenal and required the staff to master new electronic technology. Nevertheless by the end of 1970 the first research and development spacecraft was ready for launch and the RLS system was undergoing static trials. During the course of 1971-1972 all ground research and qualification tests were completed. Flight trials of the RLS began in 1973. These were successful and even test operations of the system marked a major new military capability for the VMF. The RLS was accepted for military service in 1975.

The RLS had the worst reliability and quality problems of any Soviet system. It was not available often enough for good exploitation of the data. Between 1979 and 1989 a phased modernization of the MKRTs was undertaken, providing better accuracy, localization of targets, and one-time observation capability. Flight durations were increased five to ten times. The entire surface of the world's ocean was continuously monitored, a feat not achieved by any other system. The system's effectiveness was proven in the 1982 Falklands War, when MKRTs monitored the British forces and was able to advise the General Staff of the Soviet Navy of the exact moment of the British landing.

The nuclear spacecraft component had redundant systems for placing the reactor into a safe high storage orbit at the end of spacecraft operations. The YaEU nuclear reactor was equipped with an automatic system to place it into a higher safe orbit after operations were completed.


More at: US-A.

Family: Medium earth orbit, Naval surveillance radarsat, Surveillance. Country: Russia. Engines: Stepanov IS/US 16 kgf. Launch Vehicles: R-7, UR-200, Tsiklon, Soyuz 11A510, Tsiklon-2, Tsiklon-2A. Projects: RORSAT. Launch Sites: Baikonur, Baikonur LC31, Baikonur LC90/19. Agency: MO, Arsenal. Bibliography: 102, 2, 279, 290, 376, 42, 474, 6, 7008, 13317, 13318.
Photo Gallery

USA TrackingUSA Tracking


USA Ground EquipmentUSA Ground Equipment


USA Fissile MaterialUSA Fissile Material


USA Reactor DisposalUSA Reactor Disposal


USA CovergeUSA Coverge


USA SeparationUSA Separation


Cosmos 125Cosmos 125
Credit: Manufacturer Image



1961 March 6 - . Launch Vehicle: UR-200.
1961 March 16 - . Launch Vehicle: UR-200.
1962 June 3 - . Launch Vehicle: UR-200.
1962 July - . Launch Vehicle: UR-200.
1964 June 18 - .
1964 October 13 - .
1965 August 24 - .
1965 December 27 - . 22:19 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A510.
1966 July 20 - . 09:07 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A510.
1967 July 1 - . LV Family: R-36. Launch Vehicle: Tsiklon-2.
1967 July 21 - .
1967 December 27 - . 11:28 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. LV Family: R-36. Launch Vehicle: Tsiklon-2A.
1968 March 22 - . 09:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. LV Family: R-36. Launch Vehicle: Tsiklon-2A.
1969 January 25 - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. LV Family: R-36. Launch Vehicle: Tsiklon-2A. FAILURE: Payload propulsion system failed; no orbit.. Failed Stage: P.
1970 October 3 - . 10:26 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1971 April 1 - . 11:29 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1971 December 25 - . 11:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1972 August 21 - . 10:36 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1973 April 25 - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2. FAILURE: Payload propulsion system failed; no orbit.. Failed Stage: P.
1973 December 27 - . 20:19 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1974 May 15 - . 07:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1974 May 17 - . 06:53 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1975 April 2 - . 11:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/20. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1975 April 7 - . 11:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/20. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1975 October 1 - . LV Family: R-36. Launch Vehicle: Tsiklon-2.
1975 December 12 - . 12:45 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1976 October 17 - . 18:06 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1976 October 21 - . 16:53 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1977 September 16 - . 14:25 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1977 September 18 - . 13:48 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1980 April 29 - . 11:40 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1981 March 5 - . 18:09 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1981 April 21 - . 03:45 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1981 August 24 - . 16:37 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1982 May 14 - . 19:39 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1982 June 1 - . 13:58 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1982 August 30 - . 10:06 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1982 October 2 - . 00:01 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1984 June 29 - . 00:21 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1984 October 31 - . 12:29 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1985 August 1 - . 05:36 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1985 August 23 - . 22:33 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1986 March 21 - . 10:05 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1986 August 20 - . 12:58 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1987 June 18 - . 21:33 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1987 December 12 - . 05:40 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.
1988 March 14 - . 14:21 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2.

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