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Resurs
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 | Resurs F1 Credit - © Mark Wade
| Program: Resurs. Objective: Surveillance. Type: Military. Zenit-derived satellites used for earth resources studies as part of the 'Resurs' and 'Gektor-Priroda' project. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation. Major Events:
- 1983 July 24 - Cosmos 1484. Spacecraft: Resurs-OE. Mass: 2,500 kg (5,500 lb). Launch Site: Baikonur. Launch Vehicle: Vostok 8A92M.
Follow-on to Meteor series. Second flight of prototype for Resurs-O1 spacecraft. Gathering regular information on the natural resources of the earth for use in various branches of the Soviet economy, and conducting further tests on new types of measuring apparatus and methods of remote sensing of the earth's surface and atmosphere.
- 1985 October 3 - Cosmos 1689. Spacecraft: Resurs-O1. Mass: 1,500 kg (3,300 lb). Launch Site: Baikonur. Launch Vehicle: Vostok 8A92M.
First flight of Resurs-O1. Acquisition of operational information on the natural resources of the earth in the interests of various branches of the national economy of the USSR; continued trials of new types of informational and measurement apparatus and methods of remote sensing of the earth's surface and atmosphere. Operated for one year, two months. Re-entered January 14, 2001.
- 1988 April 20 - Cosmos 1939. Spacecraft: Resurs-O1. Mass: 2,000 kg (4,400 lb). Launch Site: Baikonur. Launch Vehicle: Vostok 8A92M.
Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation. Stayed in operation for six years, six months, far beyond its rated life of 3 to 5 years.
- 1989 January 12 - Cosmos 1990. Spacecraft: Resurs F2. Mass: 6,300 kg (13,800 lb). Launch Site: Plesetsk. Launch Vehicle: Soyuz 11A511U.
Investigation of the natural resources of the earth in the interests of the national economy of the USSR and international cooperation; survey of seismically active regions of the country, including the Armenian SSR, in the interests of industrial and non -industrial construction.
- 1990 May 29 - Resurs F-06. Spacecraft: Resurs F1-14F43. Mass: 6,300 kg (13,800 lb). Launch Site: Plesetsk. Launch Vehicle: Soyuz 11A511U.
Also carried German microgravity experiment. Investigation of the natural resources of the Earth in the interests of various branches of the national economy of the USSR; solution of problems relating to ecology and international cooperation. In accordance with a commercial agreement, apparatus belo nging to the Federal Republic of Germany is also being carried for the purpose of conducting biotechnological experiments.
- 1992 November 15 - Resurs-500. Spacecraft: Resurs F1-14F43. Mass: 6,300 kg (13,800 lb). Launch Site: Plesetsk. Launch Vehicle: Soyuz 11A511U.
Carried descent module with greetings to American people. Delivery of a humanitarian cargo (messages to the American people, promotional materials of Russian and foreign firms, etc.) to the United States of America in connection with the 500th anniversary of the discovery of America by Columbus.
- 1994 November 4 - Resurs-O1 No. 3. Spacecraft: Resurs-O1. Mass: 1,900 kg (4,100 lb). Launch Site: Baikonur. Launch Vehicle: Zenit-2.
Studied natural resources. It carried the German Safir-R1 communications experiment as a secondary attached payload. Expected life 3 to 5 years. The spacecraft mass of 1,907 kg was slightly higher than earlier models. The principal Earth observation sensors were MSU-SK and MSU-E instruments along with an experimental PVM-E local vertical sensor .
- 1998 July 10 - Resurs-O1 No. 4. Spacecraft: Resurs-O1. Launch Site: Baikonur. Launch Vehicle: Zenit-2.
In addition to its remote sensing equipment, the satellite carried the Belgian LLMS (Little LEO Messaging System) communications payload for the IRIS system. The launch was critical in restoring confidence in the Zenit vehicle prior to planned commercial launches of Globalstar satellites from Baikonur and the first Sea Launch flights using a three-stage Zenit from a California-based floating launch platform. Expected life 3 to 5 years.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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