Engineering:4MV

From HandWiki
Revision as of 19:53, 4 February 2024 by NBrushPhys (talk | contribs) (url)
(diff) ← Older revision | Latest revision (diff) | Newer revision → (diff)
4MV
Mars 6.jpg
Mars-6, a 3MP version of the 4MV bus.
ManufacturerNPO Lavochkin
Country of originSoviet Union
OperatorSoviet Space Program
Specifications
Power2 Solar arrays (Mars, Venera)
4 Solar arrays (Astron, Granat)
Production
Operational1971-1989

Engines:

  • 1 KTDU-425 (Mars 2-3)
  • 1 KTDU-425A (Post 1971)
  • Fuel:
  • UDMH/N2O4
  • ← 3MV 5VK
    Short description: Design used for Soviet space probes to Mars and Venus

    The 4MV planetary probe (short for 4th-generation Mars-Venus probe) is a designation for a common design used for Soviet unmanned probes to Mars and Venus.

    It was an incremental improvement of earlier 3MV probes and was used for Mars missions 2 to 7 and Venera missions 9 to 16. Different versions of the bus exist, for example 4V-1, 4V-M and 4V-2.[1][2] The same base design was also used for earth-orbiting space observatories.[3]

    Design

    The spacecraft bus has a height of 2.8 meters (9 ft 2 in) and a solar panel span of 6.7 meters (22 ft). The central section of the bus has a diameter of about one meter (3 ft 3 in) and contained propellant. The main engine (KTDU-425) is encircled by a conical instrument compartment with the diameter of 2.35 meters (7 ft 9 in) at the base.[4] While Mars 2,3 and Kosmos 419 used the KTDU-425, 4MV buses after 1971 used the KTDU-425A).[5]

    Astron

    Variants

    M-71 - 3MS version

    See also

    References