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Proton (satellite program)
Series of Soviet satellites
Series of Soviet satellites
| Field | Value | ||||
|---|---|---|---|---|---|
| name | * Proton 1*, *2*, *3*, and *4* | ||||
| image | File:Proton1-2.gif | ||||
| image_caption | A Proton satellite | ||||
| mission_type | Astronomy | ||||
| operator | Soviet Union | ||||
| COSPAR_ID | {{plainlist | ||||
| manufacturer | OKB-52 | ||||
| launch_mass | {{plainlist | ||||
| *{{convert | 12200 | kg | lb | abbr | on}} (Proton 1) |
| *{{convert | 12200 | kg | lb | abbr | on}} (Proton 2) |
| *{{convert | 12200 | kg | lb | abbr | on}} (Proton 3) |
| *{{convert | 17000 | kg | lb | abbr | on}} (Proton 4)}} |
| launch_date | {{plainlist | ||||
| *Proton 1: {{start-date | 16 July 1965 11:16 | timezone | yes}} UTC | ||
| *Proton 2: {{start-date | 2 November 1965 12:28 | timezone | yes}} UTC | ||
| *Proton 3: {{start-date | 6 July 1966 12:57 | timezone | yes}} UTC | ||
| *Proton 4: {{start-date | 16 November 1968 11:40 | timezone | yes}} UTC}} | ||
| launch_rocket | UR-500 (1–3), Proton-K (4) | ||||
| launch_site | Baikonur Cosmodrome Site 81/23 (1–3), Baikonur Cosmodrome Site 81/24 (4) | ||||
| disposal_type | De-orbited | ||||
| decay_date | {{plainlist | ||||
| *Proton 1: {{end-date | 11 October 1965 | timezone | yes}} | ||
| *Proton 2: {{end-date | 6 February 1966 | timezone | yes}} | ||
| *Proton 3: {{end-date | 16 September 1966 | timezone | yes}} | ||
| *Proton 4: {{end-date | 24 July 1969 | timezone | yes}}}} | ||
| orbit_reference | Geocentric | ||||
| orbit_periapsis | {{plainlist | ||||
| orbit_apoapsis | {{plainlist | ||||
| *Proton 1: <ref name | nssdc1 | ||||
| *Proton 2: <ref name | nssdc2 | ||||
| *Proton 3: <ref name | nssdc3 | ||||
| *Proton 4: }}<ref name | nssdc4 | ||||
| orbit_inclination | 63.5° (1–3), 31.5° (4) | ||||
| orbit_period | ~92 minutes (1–4) | ||||
| orbit_eccentricity | .030 (1–3), .017 (4) | ||||
| apsis | gee |
-
1965-054A (Proton 1)
-
1965-087A (Proton 2)
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1966-060A (Proton 3)
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1968-103A (Proton 4)}}
-
12200 kg (Proton 1)
-
12200 kg (Proton 2)
-
12200 kg (Proton 3)
-
17000 kg (Proton 4)}}
-
Proton 1: UTC
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Proton 2: UTC
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Proton 3: UTC
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Proton 4: UTC}}
-
Proton 1:
-
Proton 2:
-
Proton 3:
-
Proton 4: }}
-
Proton 1: 183 km
-
Proton 2: 189 km
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Proton 3: 185 km
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Proton 4: 248 km}}
-
Proton 1: 589 km
-
Proton 2: 608 km
-
Proton 3: 585 km
-
Proton 4: 477 km}}
Proton () ('proton') was a Soviet series of four cosmic ray and elementary particle detecting satellites. Orbited 1965–68, three on test flights of the UR-500 ICBM and one on a Proton-K rocket, all four satellites completed their missions successfully, the last reentering the Earth's atmosphere in 1969.
Background
The Proton satellites were heavy automated laboratories launched 1965–68 to study high energy particles and cosmic rays. These satellites were built to utilize the test launches of the UR-500, a heavy two-stage ICBM designed by Vladimir Chelomey's OKB-52 to carry a 100-megaton nuclear payload. Each Proton was housed in a purpose-built third stage added to the UR-500 stack.
Spacecraft design
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Protons 1–3 were largely identical craft massing 12200 kg, with scientific packages developed under the supervision of Academician Sergey Nikolayevich Vernov of Moscow State University's Scientific-Research Institute of Nuclear Physics. The counters were able to determine the total energy of each super-high energy cosmic particle individually, a capability no prior satellite had possessed. Though the equipment had been developed eight years earlier (by Professor N. L. Grigorov), the UR-500 was the first booster powerful enough to orbit a satellite carrying the sensitive particle counter. The counters could measure cosmic rays with energy levels up to 100 million eV.
Proton 3 also was equipped with a gas-Cerenkov-scintillator telescope to attempt to detect the newly postulated fundamental particle, the quark. The entire experiment package massed 4000 kg and was composed of metal, plastic, and paraffin blocks.
Telemetry was relayed via a 19.910 MHz beacon. Four solar panels powered the crafts, which were cooled by heat exchangers. The Protons were spin-stabilized, their attitude controlled by jet and an on-board dampener. Satellite systems were controlled by an internal computer.
Proton 4 was considerably more massive at 17000 kg. Its primary instrument was an ionization calorimeter composed of steel bars and plastic scintillators. A measuring device comprising one lump of carbon and another of polyethylene provided data on cosmic rays and the energy spectrum in orbit, the possible collisions of cosmic ray particles with atmospheric nuclei of hydrogen, carbon, and iron, and continued the search for the quark.
Missions
Proton 1
Proton 1 was launched into Earth orbit 16 July 1965 11:16 UTC from Baikonur Cosmodrome Site 81/23, though the launch was threatened by a leak in the oxidizer pipeline resulting in nitrogen tetroxide spilling on electrical wires. Early in the flight, launch specialists only received signals indicating that the satellite was functioning. Eventually, however, Proton 1 performed normally, returning physics data on ultra-high-energy cosmic particles. Its mission lasted 45 days,
Proton 2
The virtually identical Proton 2 was launched 2 November 1965 12:28 UTC, also from Baikonur Cosmodrome Site 81/23.
Proton 3
After an unsuccessful launch of the third test UR-500 on 24 March 1966 14:39 UTC, Proton 3 was successfully launched into Earth orbit from Baikonur Cosmodrome Site 81/23 on 6 July 1966 12:57 UTC reentering Earth's atmosphere on 16 September 1966.
Proton 4
After the end of the run of UR-500 test launches, the rocket (now designated Proton) and its successors were largely employed in the launch of the Zond lunar spacecraft. However, on 16 November 1968 11:40 UTC, the final and much larger Proton 4 was launched into orbit via Proton-K rocket from Baikonur Cosmodrome Site 81/24 to continue the search for the quark and supplement the earlier Proton satellites' cosmic ray measurements. This final Proton reentered Earth's atmosphere on 24 July 1969.
Legacy
The Proton satellites were heralded by Soviet media as the start of a new stage in Soviet space exploration. The success of Proton afforded Chelomey a status in the Soviet rocket industry equal to that of Sergei Korolev of OKB-1 (developer of Sputnik, Vostok, and Voskhod) and Mikhail Yangel of OKB-456 (an important designer of military missiles). The UR-500, originally named "Gerkules" () ('Hercules'), was renamed "Proton" when news reports conflated the launcher and its payload. Though the Proton was never used in the ICBM role it had been built for, the rocket became an extraordinarily successful booster for commercial satellites, serving well into the 1990s.
References
References
- "Proton 1". NASA Space Science Data Coordinated Archive.
- "Proton 2". NASA Space Science Data Coordinated Archive.
- "Proton 3". NASA Space Science Data Coordinated Archive.
- "Proton 4". NASA Space Science Data Coordinated Archive.
- Wade, Mark. "UR-500".
- Chertok. (2011). "Rockets and People. Volume IV, The Moon Race". NASA.
- William R. Corliss. (1967). "Scientific Satellites". Science and Technical Information Division, Office of Technology Utilization, National Aeronautics and Space Administration.
- "Aeronautics and Astronautics, 1965". NASA.
- Hart, Douglas M.. (1987). "The Encyclopedia of Soviet Spacecraft". Exeter Books.
- Akimov, V. V.. (1970). "Measurements of the primary cosmic ray spectra in the 1011-1014 eV energy range from Proton-1, 2, 3 satellites". Proceedings of the 11th International Conference on Cosmic Rays, held in Budapest, 25 August – 4 September 1969.
- McDowell, Jonathan. "Launch Log". Jonathon's Space Report.
- McDowell, Jonathan. "Satellite Catalog". Jonathon's Space Report.
- (8 November 1965). "News Digest (Soviets launched)". McGraw Hill Publishing Company.
- "Aeronautics and Astronautics, 1965". NASA.
- Bruce S. Maccabee. (August 2000). "Gemini 11 UFO".
- (19 September 1966). "Gemini 11 Demonstrates Pilot Capabilities". McGraw Hill Publishing Company.
- Asif A. Siddiqi. "Challenge to Apollo: The Soviet Union and the Space Race, 1945–1974". NASA.
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