Kosmos 672
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| Mission type | Orbital test flight |
|---|---|
| Operator | Soviet space program |
| COSPAR ID | 1974-064A |
| SATCAT no. | 7413 |
| Mission duration | Template:Time interval |
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| Spacecraft properties | |
| Spacecraft | Soyuz 7K-TM s/n 72 |
| Manufacturer | NPO Energia |
| Launch mass | Template:Cvt |
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| Start of mission | |
| Launch date | 12 August 1974, 06:25 GMT[1] |
| Rocket | Soyuz-U |
| Launch site | Baikonur 31/6 |
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| End of mission | |
| Disposal | Deorbited |
| Landing date | 18 August 1974, 05:02 GMT[1] |
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| Orbital parameters | |
| Reference system | Geocentric |
| Perigee altitude | Template:Cvt |
| Apogee altitude | Template:Cvt |
| Inclination | 51.7° |
| Period | 88.9 min |
| Template:Succession links Template:Succession links | |
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Kosmos 672 (Template:Langx meaning Cosmos 672) was the second uncrewed test of the ASTP Soyuz spacecraft. Also had APAS-75 androgynous docking system.
This was preceded by another uncrewed test of this spacecraft type, Kosmos 638.[2] It was a Soyuz 7K-TM spacecraft.[2]
Mission parameters
- Spacecraft: Soyuz 7K-TM
- Mass: 6510 to 6680 kg
- Crew: None
- Launched: August 12, 1974
- Landed: August 18, 1974
See also
References
- ^ a b Page Module:Citation/CS1/styles.css has no content.David S. F. Portree (1995). Mir Hardware Heritage (PDF). NASA. Archived (PDF) from the original on 26 March 2023.
- ^ a b Page Module:Citation/CS1/styles.css has no content.Rex Hall; David Shayler (2003). Soyuz: A Universal Spacecraft. Springer Science & Business Media. p. 211. ISBN 978-1-85233-657-8.
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