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T-1
Part of R-7
Original conceptual design for ICBM. Final design was R-7 due to unachievability of mass ratio for this single stage design. Data from chart at Russian Space Agency HQ.

Status: Study 1953. Payload: 11,000 kg (24,000 lb). Thrust: 2.64 kN (593 lbf). Gross mass: 190,000 kg (410,000 lb). Apogee: 1,267 km (787 mi).

Maximum range: 8,000 km (4,900 mi). CEP: 12.90 km (8.00 mi). Maximum speed: 23,450 kph (14,570 mph).

Family: ICBM. Country: Russia. Agency: Korolev bureau. Bibliography: 283.
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