3MV

{{Short description|Soviet unmanned Venus and Mars probe design}}

{{use mdy dates|date=September 2021}}

{{Use American English|date=November 2020}}

{{Infobox spacecraft class|name=3MV|manufacturer=OKB-1 (Pre 1967)

NPO Lavochkin (1967-1972)|image=File:Nave_espacial_Venera_8.jpg|image_caption=Venera-8, a late model 3MV (V-72)|image_size=|country=Soviet Union|Succeeded=4MV|Preceded=2MV|operational=1963-1972|launch_mass=800-960kg (Zond/Early Types)

963kg (Venera 2)

960kg (Venera 3)

1106 kg (Venera 4)

1130 kg (Venera 5-6)

1180kg (Venera 7)

1184kg (Venera 8)|derivedfrom=2MV}}

The 3MV planetary probe (short for 3rd generation Mars-Venus) is a designation for a common design used by early Soviet unmanned probes to Mars and Venus.{{Cite web |title=3MV |url=http://www.astronautix.com/3/3mv.html |access-date=2023-09-25 |website=www.astronautix.com}} It was an incremental improvement of earlier 2MV probes and was used for Zond 1, Zond 2 and Zond 3 missions to Mars as well as several Venera probes. It was standard practice of the Soviet space program to use standardized components as much as possible. All probes shared the same typical characteristics and differed usually in equipment necessary for specific missions. Each probe also incorporated improvements based on experience with earlier missions.

Original design (1963-1965)

The probe consisted of three primary parts.

=Orbital Compartment=

The core of the stack was a pressurized compartment called the Orbital Compartment. This part housed the spacecraft's control electronics, radio transmitters and receivers, batteries, astro-orientation equipment, and so on. The compartment was pressurized to around 100 kPa and thermally controlled to simulate earth-like conditions, which removed the need for special electronic components that could reliably operate in extreme conditions (on Zond 1 the module depressurized in flight, severely damaging the probe's systems).

Image:Zond 2.jpgMounted on the outside of the Orbital Compartment were two solar panels which supplied power to the spacecraft. They were folded against the body of the probe during launch and were only deployed when the craft was already on its interplanetary trajectory. On the ends of each solar panel was a hemispherical radiator which radiated excess heat from the orbital compartment into space through a coolant loop.

Also mounted on the Orbital Compartment was a 2 m parabolic high-gain antenna, used for long-range communications. Depending on the mission, the probe also used other antennas (for example, for communication with probes on the planet's surface).

=Planetary Compartment=

Below the Orbital Compartment was a second pressurized compartment called the Planetary Compartment. Depending on the mission the Planetary Compartment either housed scientific equipment for orbital observation of the planet or was designed to detach and land on the planet's surface.

=Engine=

Course correction capabilities were provided by a KDU-414 engine attached to the top of the Orbital Compartment. It provided a maximum thrust of around 2 kN and used UDMH and nitric acid as propellants. Attitude control was achieved by several small cold gas thrusters.

The whole stack was 3.6 m high and weighted around 1000 kg.

NPO Lavochkin version (1967-1972)

In 1965, a few months before his death, OKB-1 Chief Designer Sergei Korolev switched over the role of Space Probe design and construction to aviation manufacturer NPO Lavochkin. Many changes were made to the 3MV, which began receiving the new designation system used by Lavochkin, the first one being V-67 (Venus 1967).{{Cite web |title=Plumbing the Atmosphere of Venus |url=http://mentallandscape.com/V_Lavochkin1.htm |website=mentallandscape.com|url-status=live

|archive-url=https://web.archive.org/web/20220414155856/http://mentallandscape.com/V_Lavochkin1.htm |archive-date=14 April 2022}} This included the removal of the Radiator spheres on the ends of the solar panels, replaced by the use of antennas as a radiator, increasing the size of the panels. The probe was also heavier than the previous Venera 3. This was due to the change in Soviet thinking of the possible temperature of Venus, with this leading to the V-67 lander being strengthened (although still not strong enough) for the expected harsher environment.{{Cite web |title=Inventing The Interplanetary Probe |url=http://mentallandscape.com/V_OKB1.htm |website=mentallandscape.com |url-status=live |archive-url=https://web.archive.org/web/20220408052534/http://mentallandscape.com/V_OKB1.htm |archive-date=8 April 2022}} It was also equipped with an ablative heat shield.*

After Venera 4's failure to reach the surface of Venus intact, the next 3MV probes (Venera 5 and 6) were strengthened again, this time to withstand a 450-g (compared to the 300-g entry of Venera 4) re-entry due to the 1969 launch window's higher velocity. The V-70 design took this further, with the capsule being slightly more egg-shaped. It was designed to survive 150 atmospheres and 540°C (1004°F). The Parachute was also changed to the heavier weight and the lander was set to -8°C before detaching from the 3MV bus. Due to these changes, Venera-7 became the first spacecraft to land on Venus, and another planet successfully. The final version of the 3MV bus, the V-72 probes, were launched in early 1972, with one failing to reach Venus (Kosmos 482 which was still orbiting Earth as of 2011).{{Cite web |title=Kosmos-482 (Venera-72 No. 2) mission |url=http://www.russianspaceweb.com/venera72_kosmos482.html |website=www.russianspaceweb.com |url-status=live |archive-url=https://web.archive.org/web/20220414155714/http://www.russianspaceweb.com/venera72_kosmos482.html |archive-date=14 April 2022}} The 3MV was superseded by the newer 4V-1 probes beginning in 1975 with Venera 9 and 10, based on the M-71/73 probes (Mars-2-7).{{Cite web |title=First Pictures of the Surface of Venus |url=http://mentallandscape.com/V_Lavochkin2.htm |website=mentallandscape.com |url-status=live |archive-url=https://web.archive.org/web/20220414155855/http://mentallandscape.com/V_Lavochkin2.htm |archive-date=14 April 2022}}{{Cite web |title=Venera-9 and 10 |url=http://www.russianspaceweb.com/venera75.html#history |website=www.russianspaceweb.com |url-status=live |archive-url=https://web.archive.org/web/20220408162710/http://www.russianspaceweb.com/venera75.html#history |archive-date=8 April 2022}}

Variants

  • Venera 3MV-1A: Kosmos 21 (3MV-1 No.1), 3MV-1A (failure){{Cite web |title=Zond (3MV-1A #1, 2) |url=https://space.skyrocket.de/doc_sdat/zond-3mv-1a.htm |access-date=2023-09-25 |website=Gunter's Space Page |language=en}}
  • Venera 3MV-1: Zond 3MV-1 No.2 (failure), Kosmos 27 (3MV-1 No.3), Zond 1 (3MV-1 No.4)){{Cite web |title=Zond 1 (3MV-1 #1, 2) |url=https://space.skyrocket.de/doc_sdat/zond-3mv-1.htm |access-date=2023-09-25 |website=Gunter's Space Page |language=en}}
  • Mars 3MV-4A: Zond 2 (3MV-4A No.2), Zond 3 (3MV-4A No.3){{Cite web |title=Zond 2, 3 / Venera 2 (3MV-4 #1, 2, 3, 4) |url=https://space.skyrocket.de/doc_sdat/venera-3mv-4.htm |access-date=2023-09-25 |website=Gunter's Space Page |language=en}}
  • Venera 3MV-4: Venera 2 (3MV-4 No.4), Kosmos 96 (3MV-4 No.6)
  • Venera 3MV-3: Venera 3 (3MV-3 No.1), Venera 3MV-3{{Cite web |title=Venera 3 (3MV-3 #1) |url=https://space.skyrocket.de/doc_sdat/venera-3mv-3.htm |access-date=2023-09-25 |website=Gunter's Space Page |language=en}}
  • Venera 3V (V-67): Venera 4 (V-67 No. 310), Kosmos 159 (V-67 No.311){{Cite web |title=Venera 4 (V-67 #1, 2) |url=https://space.skyrocket.de/doc_sdat/venera-v67.htm |access-date=2023-09-25 |website=Gunter's Space Page |language=en}}
  • Venera 3V (V-69) Venera 5 (V-69 No. 330), Venera 6 (V-69 No. 331){{Cite web |title=Venera 5, 6 (V-69 #1, 2) |url=https://space.skyrocket.de/doc_sdat/venera-v69.htm |access-date=2023-09-25 |website=Gunter's Space Page |language=en}}
  • Venera 3V (V-70): Venera 7 (V-70 No.630), Kosmos 359 (V-70 No.631){{Cite web |title=Venera 7 (V-70 #1, 2) |url=https://space.skyrocket.de/doc_sdat/venera-v70.htm |access-date=2023-09-25 |website=Gunter's Space Page |language=en}}
  • Venera 3V (V-72): Venera 8 (V-72 No.670), Kosmos 482 (V-72 No.671){{Cite web |title=Venera 8 (V-72 #1, 2) |url=https://space.skyrocket.de/doc_sdat/venera-v72.htm |access-date=2023-09-25 |website=Gunter's Space Page |language=en}}

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See also

References

{{Reflist}}

  • [https://web.archive.org/web/20120808012346/http://files.seds.org/pub/info/newsletters/ejasa/1991/jasa9104.txt "The Mystery of Zond 2"] by Andrew Lepage, EJASA, April 1991, retrieved on January 21, 2012
  • [http://www.russianspaceweb.com/spacecraft_planetary_venus.html "The overview of the Russian launches toward Venus"] by Anatoly Zak, July 2007, retrieved on December 2, 2007
  • [https://web.archive.org/web/20100720011556/http://www.russianspaceweb.com/spacecraft_planetary_mars.html "The overview of the Russian launches toward Mars"] by Anatoly Zak, August 2007, retrieved on December 2, 2007

Category:Soviet Mars missions

Category:Soviet Venus missions

Category:Soviet space probes

{{USSR space probes}}