Kosmos 300

Failed Soviet lunar sample-return mission
Kosmos 300
OperatorSoviet space program
COSPAR ID1969-080A Edit this at Wikidata
SATCAT no.4104
Mission duration4 days
Spacecraft properties
Spacecraft typeYe-8-5
ManufacturerGSMZ Lavochkin
Launch mass5,600 kg (12,300 lb)[1]
Start of mission
Launch dateSeptember 23, 1969, 14:07:00 (1969-09-23UTC14:07Z) UTC[2]
RocketProton-K/D
Launch siteBaikonur 81/24
End of mission
DisposalLaunch failure
Decay dateSeptember 27, 1969
Orbital parameters
Reference systemGeocentric[2]
Perigee altitude184 km (114 mi)
Apogee altitude189 km (117 mi)
Inclination51.5°
Period88.2 min
Luna programme
← Luna 15
Kosmos 305 →
 
Kosmos (satellites)
← Kosmos 299
Kosmos 301 →

Kosmos 300 (Russian: Космос 300 meaning Cosmos 300) (Ye-8-5 series) was the fourth Soviet attempt at an uncrewed lunar sample return. It was probably similar in design to the later Luna 16 spacecraft. It was launched, on a Proton rocket, on September 23, 1969.[3] The mission was a failure. The engines on the Block D upper stage failed due to an oxidizer leak, leaving the spacecraft to burn up in Earth's atmosphere.[4]

References

  1. ^ "NASA NSSDC Master Catalog - Cosmos 300". Retrieved 25 May 2024.
  2. ^ a b "Luna Ye-8-5 - Encyclopedia Astronautica". Retrieved 25 May 2024.
  3. ^ "Luna - Exploring the Moon". orbitalfocus.uk. Retrieved February 23, 2023.
  4. ^ Siddiqi, Asif A. (2018). "Kosmos 300 [Luna]" (PDF). Beyond Earth: A Chronicle of Deep Space Exploration, 1958-2016. NASA History Program Office: 92. Retrieved February 23, 2023.
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Orbital launches in 1969
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets).


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