astronautix.com | Chronology - 1982 - Quarter 4 |
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Ocean surveillance; nuclear powered. References: 1 , 2 , 5 , 6 .
Glonass test flight. Testing of the components and equipment of the space navigation system established in order to locate the Soviet Union's civil aircraft and its merchant and fishing vessels. Three satellites launched by a single carrier rocket. References: 1 , 2 , 5 , 6 , 67 , 274 .
Glonass test flight. Testing of the components and equipment of the space navigation system established in order to locate the Soviet Union's civil aircraft and its merchant and fishing vessels. Three satellites launched by a single carrier rocket. References: 1 , 2 , 5 , 6 , 67 , 274 .
Glonass test flight. Testing of the components and equipment of the space navigation system established in order to locate the Soviet Union's civil aircraft and its merchant and fishing vessels. Three satellites launched by a single carrier rocket. References: 1 , 2 , 5 , 6 , 67 , 274 .
Photo surveillance; returned film capsule; maneuverable. References: 1 , 2 , 6 .
Military navigation satellite. Replaced Cosmos 1308. References: 1 , 2 , 5 , 6 .
Stationed at 90 deg E. Provision of telephone and telegraph radiocommunications and transmission of television programmes. References: 1 , 2 , 5 , 6 , 67 , 111 , 274 .
Radar calibration mission. References: 1 , 2 , 5 , 6 .
Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
Spent boosters, spent maneuvering stages, shrouds and other non-functional objects (US Cat D). References: 1 , 2 , 5 , 6 .
Unmanned supply vessel to Salyut 7. Docked with Salyut 7 on 2 Nov 1982 13:22:00 GMT. Undocked on 13 Dec 1982 15:32:00 GMT. Destroyed in reentry on 14 Dec 1982 17:17:00 GMT. Total free-flight time 3.16 days. Total docked time 41.09 days. References: 1 , 2 , 6 , 275 .
Photo surveillance; returned film capsule; maneuverable. References: 1 , 2 , 6 .
Deployed from STS-5 11/11/82. Telecommunications. Operating entity Telesat Canada. Longitude 117.5W. Transmit power 11.2 W per frequency at input of transmit antenna (typical saturated carrier). Anik C-3 Transmit frequency (MHz): 11730, 11743, 11791, 11804, 11852 , 11865, 11913, 11926, 11974, 11987, 12035, 12048, 12096, 12109 , 12157, 12170. References: 1 , 2 , 5 , 6 .
Deployed from STS-5 11/11/82. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
Manned four crew. First mission to deploy commercial communications satellites (SBS 3, Anik C3). Payloads: : Satellite Business Systems (SBS)-C with Payload Assist ; (PAM)-D; Telesat-E (Canadian communications satellite) with PAM-D. Monodisperse Latex Reactor (MLR), Continuous Flow Electrophoresis System (CFES), three getaway specials (GAS), Student experiments, GLOW experiment, Vestibular experiment, Oxygen Interaction With Materials experiment. Additional Details: STS-5. References: 1 , 2 , 5 , 6 , 7 , 33 .
Final launch of a Titan IIID from Vandenberg AFB (first launch on 1 5 June 1971). References: 88 .
KH-11 type satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
Photo surveillance; returned film capsule; maneuverable. References: 1 , 2 , 6 .
Launched from Salyut 7 airlock. Conduct of experiments in the field of amateur radiocommunications. References: 1 , 2 , 6 .
Provision of uninterrupted round the clock telephone and telegraph radiocommunication in the USSR and simultaneous transmission of colour and black-and-white USSR central television programmes to stations in the Orbita network. References: 1 , 2 , 5 , 6 , 67 , 274 .
During 1982 the 3M-T transport aircraft was completed and began delivery of central block propellant tanks and structural elements for construction of a realistic mock-up of the booster.
Photo surveillance; returned film capsule; maneuverable. References: 1 , 2 , 6 .
Intended to replace Molniya 1-48; failed. Investigation of the upper atmosphere and outer space. References: 1 , 2 , 5 , 6 , 64 , 65 .
Possible replacement for Meteor 2-6. Gathering meteorological information and data on penetrating radiation fluxes in circumterrestrial space. References: 1 , 2 , 6 .
High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission. References: 1 , 2 , 6 , 69 .
Defense Meteorological Satellite Program. References: 1 , 2 , 5 , 6 , 278 .
Photo surveillance; returned film capsule. References: 1 , 2 , 6 .
Photo/digital surveillance. References: 1 , 2 , 6 .
Radar calibration mission. References: 1 , 2 , 5 , 6 .
The 3M-T transport aircraft was completed and began delivery of central block propellant tanks and structural elements for construction of a realistic mock-up of the Energia booster. The 3M-T was a heavily modified M-4 bomber, and was limited to 50 tonnes loads carried on the top of the fuselage.
The 4M Energia launch vehicle high fidelity mock-up was completed at Baikonur.
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