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{{Short description|Unmanned test flight of the Soyuz 7K-S spacecraft}}
'''Kosmos 670''' ({{lang-ru|Космос 670}} meaning '''Cosmos 670''') was an unmanned Soyuz 7K-S test.
{{Infobox spaceflight
<!--Basic details-->
| name = Kosmos 670
| image =
| image_caption =

| mission_type = Orbital test flight
| operator = Soviet space program
| COSPAR_ID = 1974-061A
| SATCAT = 7405
| mission_duration = {{time interval|6 Aug 1974 00:02|8 Aug 1974 23:59|show=dhm}}

<!--Spacecraft properties-->
| spacecraft_type = [[Military Soyuz|Soyuz 7K-S]] s/n 1L
| manufacturer = [[NPO Energia]]
| launch_mass = {{Convert|6700|kg|abbr=on}}

<!--Launch details-->
| launch_date = {{start date text|6 August 1974, 00:02|timezone=yes}}&nbsp;GMT
| launch_rocket = [[Soyuz-U]]
| launch_site = [[Baikonur Cosmodrome|Baikonur]] [[Gagarin's Start|1/5]]

<!--end of mission-->
| disposal_type = Deorbited
| landing_date = {{end date text|8 August 1974, 23:59|timezone=yes}}&nbsp;GMT

<!--orbit parameters-->
<!--as science-related articles, SI units should be the principal units of measurement, however we usually use {{convert}} to display imperial units in parentheses after the initial values-->
| orbit_reference = [[Geocentric orbit|Geocentric]]
| orbit_periapsis = {{convert|211|km|mi|0|abbr=on}}
| orbit_apoapsis = {{convert|294|km|mi|0|abbr=on}}
| orbit_inclination = 50.6°
| orbit_period = 89.5 min
| apsis = gee

<!--Only use where a spacecraft/mission is part of a clear programme of sequential missions.
If in doubt, leave it out-->
| programme = '''[[Soyuz programme]]'''
| previous_mission = [[Soyuz 14]]
| next_mission = [[Kosmos 672]]
| programme2 = '''[[List of Kosmos satellites (501-750)|Kosmos (satellites)]]'''
| previous_mission2 = [[Kosmos 669]]
| next_mission2 = [[Kosmos 671]]
}}
'''Kosmos 670''' ({{lang-ru|Космос 670}} meaning ''Cosmos 670'') was an [[unmanned space mission|unmanned]] [[Soyuz (spacecraft)|Soyuz]] [[Military_Soyuz#Soyuz_7K-S|7K-S test]]. It used a new and unique inclination of 50.6 degree. <ref>{{Cite web |url=http://www.friends-partners.org/partners/mwade/craft/soyuz7ks.htm |title=www.friends-partners.org |access-date=2006-02-03 |archive-url=https://web.archive.org/web/20080724205431/http://www.friends-partners.org/partners/mwade/craft/soyuz7ks.htm |archive-date=2008-07-24 |url-status=dead }}</ref> The experience from these flights were used in the development of the successor program Soyuz spacecraft the [[Soyuz 7K-ST]].<ref>{{Cite web |url=http://www.friends-partners.org/partners/mwade/craft/soyuz7ks.htm |title=friends-partners.org soyuz7ks |access-date=2006-02-03 |archive-url=https://web.archive.org/web/20080724205431/http://www.friends-partners.org/partners/mwade/craft/soyuz7ks.htm |archive-date=2008-07-24 |url-status=dead }}</ref> <ref>[https://web.archive.org/web/20160820192227/http://www.astronautix.com/s/soyuz7k-s.html astronautix.com soyuz7k-s]</ref><ref name="JANE">{{cite web|url=http://www.janes.com/aerospace/civil/news/jsd/jsd030203_3_n.shtml|title=A brief history of space accidents|publisher=[[Jane's Information Group|Jane's Transport Business News]]|archive-url=https://web.archive.org/web/20030204073904/http://www.janes.com/aerospace/civil/news/jsd/jsd030203_3_n.shtml|date=February 3, 2003|archive-date=2003-02-04|access-date=2007-10-20}}</ref><ref>{{Cite news|url=https://www.bbc.com/news/world-europe-45822845|title=Astronauts escape malfunctioning rocket|date=2018-10-11|work=BBC News|access-date=2018-10-11|language=en-GB}}</ref><ref>{{cite web|url=http://ston.jsc.nasa.gov/collections/TRS/_techrep/TM-2000-209764.pdf|format=PDF|date=March 2000|page=8|title=A Human Factors Evaluation of a Methodology for Pressurized Crew Module Acceptability for Zero-Gravity Ingress of Spacecraft|last=Sanchez|first=Merri J.|publisher=[[Lyndon B. Johnson Space Center]]|location=Houston, Texas|access-date=2007-10-20|url-status=dead|archive-url=https://web.archive.org/web/20061005121847/http://ston.jsc.nasa.gov/collections/TRS/_techrep/TM-2000-209764.pdf|archive-date=2006-10-05}}</ref><ref name="americaspace">{{cite web|url=http://www.americaspace.com/?p=42882 |date=September 28, 2013|title='We Were Swearing!' Thirty Years Since Russia's Brush With Disaster|last=Evans|first=Ben|access-date=2014-01-24}}</ref>


==Mission parameters==
==Mission parameters==
*Spacecraft: 7K-S
*[[Spacecraft]]: 7K-S
*Mass: 6700 kg
*Mass: 6700 kg
*Crew: None
*Crew: None
*Launched: August 6, 1974
*Launched: August 6, 1974
*Landed: August 8, 1974 23:59 GMT.
*Landed: August 8, 1974 23:59 UTC.
*Perigee: 221 km
*Perigee: 221 km
*Apogee: 294 km
*Apogee: 294 km
*Inclination: 50.6 deg
*Inclination: 50.6 deg
*Duration: 2.99 days
*Duration: 2.99 days

==See also==
*[[Cosmos 772]]
*[[Cosmos 869]]


==References==
==References==
{{reflist}}
*http://www.friends-partners.org/partners/mwade/craft/soyuz7ks.htm




{{Portal|Spaceflight}}
{{Soyuz}}
{{Soyuz}}
{{Orbital launches in 1974}}


[[Category:Kosmos satellites|Kosmos 0670]]
[[Category:Kosmos satellites|Kosmos 0670]]
[[Category:1974 in the Soviet Union]]
[[Category:1974 in the Soviet Union]]
[[Category:Spacecraft launched in 1974]]

[[Category:Soyuz uncrewed test flights]]


{{USSR-spacecraft-stub}}
{{USSR-spacecraft-stub}}

[[cs:Kosmos 670]]
[[de:Kosmos 670]]
[[it:Cosmos 670]]
[[mk:Космос-670]]
[[ja:コスモス670号]]
[[sr:Космос-670]]

Latest revision as of 22:57, 14 June 2024

Kosmos 670
Mission typeOrbital test flight
OperatorSoviet space program
COSPAR ID1974-061A Edit this at Wikidata
SATCAT no.7405
Mission duration2 days, 23 hours and 57 minutes
Spacecraft properties
Spacecraft typeSoyuz 7K-S s/n 1L
ManufacturerNPO Energia
Launch mass6,700 kg (14,800 lb)
Start of mission
Launch date6 August 1974, 00:02 (1974-08-06UTC00:02Z) GMT
RocketSoyuz-U
Launch siteBaikonur 1/5
End of mission
DisposalDeorbited
Landing date8 August 1974, 23:59 (1974-08-09UTC00:00Z) GMT
Orbital parameters
Reference systemGeocentric
Perigee altitude211 km (131 mi)
Apogee altitude294 km (183 mi)
Inclination50.6°
Period89.5 min

Kosmos 670 (Russian: Космос 670 meaning Cosmos 670) was an unmanned Soyuz 7K-S test. It used a new and unique inclination of 50.6 degree. [1] The experience from these flights were used in the development of the successor program Soyuz spacecraft the Soyuz 7K-ST.[2] [3][4][5][6][7]

Mission parameters

[edit]
  • Spacecraft: 7K-S
  • Mass: 6700 kg
  • Crew: None
  • Launched: August 6, 1974
  • Landed: August 8, 1974 23:59 UTC.
  • Perigee: 221 km
  • Apogee: 294 km
  • Inclination: 50.6 deg
  • Duration: 2.99 days

See also

[edit]

References

[edit]
  1. ^ "www.friends-partners.org". Archived from the original on 2008-07-24. Retrieved 2006-02-03.
  2. ^ "friends-partners.org soyuz7ks". Archived from the original on 2008-07-24. Retrieved 2006-02-03.
  3. ^ astronautix.com soyuz7k-s
  4. ^ "A brief history of space accidents". Jane's Transport Business News. February 3, 2003. Archived from the original on 2003-02-04. Retrieved 2007-10-20.
  5. ^ "Astronauts escape malfunctioning rocket". BBC News. 2018-10-11. Retrieved 2018-10-11.
  6. ^ Sanchez, Merri J. (March 2000). "A Human Factors Evaluation of a Methodology for Pressurized Crew Module Acceptability for Zero-Gravity Ingress of Spacecraft" (PDF). Houston, Texas: Lyndon B. Johnson Space Center. p. 8. Archived from the original (PDF) on 2006-10-05. Retrieved 2007-10-20.
  7. ^ Evans, Ben (September 28, 2013). "'We Were Swearing!' Thirty Years Since Russia's Brush With Disaster". Retrieved 2014-01-24.