Mavr

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Status: Study 1963. Gross mass: 75,000 kg (165,000 lb). Specific impulse: 350 s. Height: 25.00 m (82.00 ft). Span: 12.00 m (39.00 ft).

This would reduce both flight time and the earth-return velocity. The project was given the code name "Mavr" ('Moor' or MArs - VeneRa).

Crew Size: 3.

Mavr Spacecraft MAVR Mars-Venus flyby spacecraft. The original TMK was similar. Credit: © Mark Wade

TMK Mars flyby TMK Mars flyby spacecraft Credit: © Mark Wade

Mavr Mavr manned Mars / Venus flyby spacecraft - 1960 Credit: © Mark Wade

Mavr Mavr spacecraft model at TsNIIMASH. The TMK-1 was similar Credit: © Mark Wade

• Lox/LH2 upper stages for the N1 necessary to achieve program - . Related Persons: Mishin, Chelomei, . Spacecraft: , MKBS, MAVR, Almaz, Salyut, LK, L3M.

  Mishin reviews the work and configurations of the Lox/LH2 (S and Sr) upper stages for the N1 necessary to achieve various programs. Mishin reviews the work and configurations of the Lox/LH2 (S and Sr) upper stages for the N1 necessary to achieve various programs (Mishin Diaries 2-293). Here was see evidence for several previously hinted-at but poorly-documented projects: the Lunar Orbital Station (N1+Almaz), the MAVR manned Mars-Venus-Flyby Spacecraft: AM Isaev - about speeding work on the engine 11D56. AM Lyulka - about speeding work on the engine 11D57.
  1. S, Sr - LOS (lunar orbital station?) SNTV satellite for direct TV broadcasting, MAVT (MAVR?), DOS-II (later Mir).
  2. S + Sr - L3M, Mavr, MKBS
  3. S + S + Sp - L3M, MKBS, Mavr and others.
  4. NII - DOS (20t - indecipherable) - this apparently refers to later plans to dump Chelomei's Proton vehicle and go back to the original plan to use the NII (consisting of the second and third stages of the N1) for this earth orbit payload class.
  5. N1S => 110 t (the low earth payload for this version of the improved N1). (Mishin Diaries 2-293).