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Displaying 21—30 of 911 matches for query "COSMOS_XXXIV" retrieved in 0.001 sec with these stats:
- "cosmo" found 1420 times in 908 documents
- "xxxiv" found 14 times in 9 documents
... (818.3-mi) perigee, 113.8-min period, and 74° inclination. Others entered following orbits: Cosmos 412, 1536-km (954.4-mi) apogee, 1482-km (920.9-mi) perigee, 116.1-min period, and 74° inclination; Cosmos 413, 1508-km (937-mi) apogee, 1476-km (917.2-mi) perigee, 115.7-min period, and 74° inclination; Cosmos 414, 1495-km (928.9-mi) apogee, 1428-km (887.3-mi) perigee, 1151-min ...
... onboard propulsion system in Apollo CSMs. Other launches identified by experts were Cosmos 379, Nov. 24; Cosmos 382, Dec. 2; and Cosmos 398, Feb. 26. Crucial hardware believed to be missing from launches ... farther in space than previous Soviet flights testing manned spaceflight equipment; at least three, including Cosmos 434, had demonstrated greater ability to maneuver in space than any previous Soviet manned flight ...
... with single booster. Tass reported Oct. 14 that equipment was functioning normally. Orbital parameters were:
Cosmos 444, 1510-km (938.3-mi) apogee, 1323-km (822.1-mi) perigee, 114.1 ... -mi) apogee, 1383-km (859.4-mi) perigee, 114.8-min period, and 74° inclination:
Cosmos 447, 1516-km (942-mi) apogee, 1412-km (877.4-mi) perigee, 115.1-min period, and 74° inclination.
Cosmos 448, 1518-km (943.2-mi) apogee, 1442-km (896-mi) perigee, 115.5-min ...
... News for this day. (1MB PDF)
U.S.S.R. launched eight Cosmos satellites from Plesetsk with single booster. Cosmos 504 entered orbit with 1497-km (930.2-mi) apogee, 1323-(822 ... -mi) apogee, 1354-km (841.4-mi) perigee, 114.3-min period, and 74° inclination. Cosmos 506 entered orbit with 1498-km (930.8-mi) apogee, 1384- km (860-mi) perigee, 114.6-nun period, and 74° inclination. Cosmos 507 entered orbit with 1497-km (930.2-mi) apogee, 1414-km (878.6-mi ...
... ) apogee, 1368- km (850.1-mi) perigee, 114.1-min period, and 74.0° inclination. Cosmos 529 entered orbit with 1469-km (912.8-mi) apogee, 1404- km (872.4-mi) perigee, 114.5-min period, and 74.0° inclination. Cosmos 530 entered orbit with 1469-km (912.8-mi) apogee, 1335-km (829.5-mi ... ) apogee, 1318-km (819.0-mi) perigee, 113.6-min period, and 74.0° inclination. Cosmos 534 entered orbit with 1469-km (912.8-mi) apogee, 1351- km (839.5-mi ...
... .pdf Space News for this day. (1MB PDF)
The U.S.S.R. launched eight Cosmos satellites-believed by Western specialists to be a military communications data-relay system-on a single booster from Plesetsk . The satellites entered earth orbit: Cosmos 564, with a 1482-km (920.9-mi) apogee, 1397-km (868.1-mi) perigee, 114.6-min period, and 74.0° inclination. Cosmos 565, with a 1493-km (927.7-mi) apogee, 1448-km (899.7-mi) perigee ...
... ) apogee, 1460-km (907.2-mi) perigee, 115.4-min period, and 74.0° inclination. Cosmos 621-1487-km (924-mi) apogee, 1407-km (874.3-mi) perigee, 114.8-min period, and 74.0° inclination. Cosmos 622-1487-km (924-mi) apogee, 1371-km (851.9-mi) perigee, 114.3-min period, and 74.0° inclination. Cosmos 623-1487-km (924-mi) apogee, 1389-km (863.1-mi) perigee, 114.5-min ...
... , in its second eight-satellite launch of the year see 23 April . Orbital parameters were:
Cosmos 677-1466-km apogee, 1398-km perigee, 114.5-min period, and 74.0° inclination ... perigee, 116.0-min period, 74.0° inclination.
Cosmos 679-1511-km apogee, 1466-km perigee, 115.8-min period, 74.0° inclination.
Cosmos 680-1492-km apogee, 1466-km perigee, 115.5-min period, 74.0° inclination.
Cosmos 681-1472-km apogee, 1466-km perigee, 115 ...
... center and crew on the orbiting complex guided search for the satellite, approach, and mooring.
Cosmos 1686 delivered equipment and various other cargo for continued functioning of the complex; the cosmonauts ... orbital complexes of large dimensions and masses.
Soviet science correspondent Boris Belitskiy said of the Cosmos 1686 mission: “The experience gained in recent years in operating such modular spacecraft with the ...
Cosmos CLXXXII was successfully launched by U.S.S.R. Orbital parameters: apogee, 355 km (221 ... , A17)''
Three possible military reasons why U.S.S.R. used one-orbit spacecraft in Cosmos series during period from Sept. 17, 1966, through Aug. 8, 1967, when seven were launched ... Nov. 2, both unannounced, and five in 1967. Cosmos CXXXIX Jan. 25, Cosmos CLX May 17, Cosmos CLXIX July 17, Cosmos CLXX July 31, and Cosmos CLXXI Aug. 8. First two in series had exploded ...
Additional database time was 0.038 sec.
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