| Mavr | ||
A variation of the TMK-1 scenario by Maksimov's unit would still use a single N1 launch. However a flyby of Venus would be undertaken on the return voyage from Mars. 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. Design Life: 680 days. Length: 25.00 m (82.00 ft). Maximum Diameter: 6.00 m (19.60 ft). Span: 12.00 m (39.00 ft). Mass: 75,000 kg (165,000 lb). Main Engine Propellants: Lox/Kerosene. Main Engine Isp: 350 sec. Electrical System: Solar panels, solar thermal. Associated Launch Vehicle: N1.
| ||
|
Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2007 except where otherwise noted. |
|
Encyclopedia Astronautica topic index 0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z |