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{{Short description|Soviet unmanned Venus and Halley comet probe design}}
The 5VK planetary probe (short for 5th-generation Venus-Comet probe) is a designation for a common design used for [[Soviet]] unmanned [[space probes|probes]] to comet [[1P/Halley]] and [[Venus]]<ref>http://www.astronautix.com/v/vega5vk.html</ref><ref>https://books.google.pt/books?id=dr6R51cqQ6IC&pg=PA638&lpg=PA638&dq=5KV+vega&source=bl&ots=sZoBcPz6pI&sig=ACfU3U2IzlKHoIb4F0gA9Lp9oxEFjPsULg&hl=pt-PT&sa=X&ved=2ahUKEwjE1vXq-avzAhWhx4UKHdeCAYMQ6AF6BAghEAM#v=onepage&q=5KV%20vega&f=false</ref>. It was an incremental improvement of earlier 4MV probes and was used for Mars and Venis missions.
{{Infobox spacecraft class
| name = 5VK
| country = [[Soviet Union]]
| operator = [[Soviet Space Program]]
| manufacturer = [[OKB-1]]
| Succeeded =
| Preceded = [[4MV]]
| image = File:Vega model - Udvar-Hazy Center.JPG
| image_caption = Vega solar system probe bus and landing apparatus (model) - Udvar-Hazy Center
}}


The '''5VK''' planetary probe (short for '''5th-generation Venus-Comet probe''') is a designation for a common design used for [[Soviet]] unmanned [[space probes|probes]] to comet [[1P/Halley]] and [[Venus]].<ref>{{Cite web|url=http://www.astronautix.com/v/vega5vk.html|archive-url=https://web.archive.org/web/20160819185117/http://www.astronautix.com/v/vega5vk.html|url-status=dead|archive-date=August 19, 2016|title=Vega 5VK|website=www.astronautix.com}}</ref><ref>{{Cite book|url=https://books.google.com/books?id=dr6R51cqQ6IC&dq=5KV+vega&pg=PA638|title=Space Flight: History, Technology, and Operations|first=Lance K.|last=Erickson|date=October 2, 2010|publisher=Rowman & Littlefield|isbn=9780865874190|via=Google Books}}</ref><ref name=":0">{{Cite web |title=Vega 1, 2 (5VK #1, 2) |url=https://space.skyrocket.de/doc_sdat/vega-1.htm |access-date=2023-09-25 |website=Gunter's Space Page |language=en}}</ref>
==Desing==
⚫
The craft was three-axis stabilized<ref>http://arc.iki.rssi.ru/IPL/vega.html</ref> and powered by twin large solar panels, weighing 4,920 kg (10,850 lb). They were equipped with a dual bumper shield for dust protection from Halley's comet. Instruments included an antenna dish, cameras, spectrometer, infrared sounder, magnetometers, and plasma probes.<ref>https://pdssbn.astro.umd.edu/data_sb/missions/vega1/index.shtml</ref><ref>http://arc.iki.rssi.ru/IPL/vega.html</ref>


It was an incremental improvement of earlier [[4MV]] probes used for [[Mars]] and Venus missions.
⚫
==Variants ==
⚫
* [[Vega 1]] (5VK No. 901)
⚫
* [[Vega 2]] (5VK No. 902)


==Design==
⚫
The craft was [[three-axis stabilized]]<ref name="auto">{{Cite web|url=http://arc.iki.rssi.ru/IPL/vega.html|title=VEGA Mission|website=arc.iki.rssi.ru}}</ref> and powered by twin large solar panels, weighing 4,920 kg (10,850 lb). They were equipped with a dual bumper shield for dust protection from Halley's comet. Instruments included an antenna dish, cameras, [[spectrometer]], infrared sounder, [[magnetometer]]s, and plasma probes.<ref>{{Cite web|url=https://pdssbn.astro.umd.edu/data_sb/missions/vega1/index.shtml|title=SBN Mission Support: Vega 1|website=pdssbn.astro.umd.edu}}</ref><ref name="auto"/>


⚫
==Variants ==
⚫
* [[Vega 1]] (5VK No.901)<ref name=":0" />
⚫
* [[Vega 2]] (5VK No.902)<ref name=":0" />

{{Commons}}


== See also ==
== See also ==
* [[Soviet space program]]
* [[Soviet space program]]
* [[Vega progam]]
* [[Vega program]]
* [[4MV]]
* [[4MV]]



==References==
==References==
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[[Category:Soviet Venus missions]]
[[Category:Soviet Venus missions]]
[[Category:Soviet space probes]]
[[Category:Soviet space probes]]

{{USSR space probes}}

Latest revision as of 23:18, 25 September 2023

5VK
Vega solar system probe bus and landing apparatus (model) - Udvar-Hazy Center
ManufacturerOKB-1
Country of originSoviet Union
OperatorSoviet Space Program
← 4MV

The 5VK planetary probe (short for 5th-generation Venus-Comet probe) is a designation for a common design used for Soviet unmanned probes to comet 1P/Halley and Venus.[1][2][3]

It was an incremental improvement of earlier 4MV probes used for Mars and Venus missions.

Design

[edit]

The craft was three-axis stabilized[4] and powered by twin large solar panels, weighing 4,920 kg (10,850 lb). They were equipped with a dual bumper shield for dust protection from Halley's comet. Instruments included an antenna dish, cameras, spectrometer, infrared sounder, magnetometers, and plasma probes.[5][4]

Variants

[edit]
Wikimedia Commons has media related to 5VK.

See also

[edit]

References

[edit]
  1. ^ "Vega 5VK". www.astronautix.com. Archived from the original on August 19, 2016.
  2. ^ Erickson, Lance K. (October 2, 2010). Space Flight: History, Technology, and Operations. Rowman & Littlefield. ISBN 9780865874190 – via Google Books.
  3. ^ a b c "Vega 1, 2 (5VK #1, 2)". Gunter's Space Page. Retrieved 2023-09-25.
  4. ^ a b "VEGA Mission". arc.iki.rssi.ru.
  5. ^ "SBN Mission Support: Vega 1". pdssbn.astro.umd.edu.
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