![]() A Ye-8-5 model in the Museum of Cosmonautics, Moscow. | |
Operator | Soviet space program |
---|---|
COSPAR ID | 1969-092A |
SATCAT no. | 4150 |
Mission duration | 2 days |
Spacecraft properties | |
Spacecraft type | Ye-8-5 |
Manufacturer | GSMZ Lavochkin |
Launch mass | 5,600 kg (12,300 lb)[1] |
Start of mission | |
Launch date | October 22, 1969, 14:09:00[2] | UTC
Rocket | Proton-K/D |
Launch site | Baikonur 81/24 |
End of mission | |
Disposal | Launch failure |
Decay date | October 24, 1969 |
Orbital parameters | |
Reference system | Geocentric[2] |
Perigee altitude | 182 km (113 mi) |
Apogee altitude | 208 km (129 mi) |
Inclination | 51.4° |
Period | 88.4 min |
Kosmos 305 (Russian: Космос 305 meaning Cosmos 305) (Ye-8-5 series) was the fifth Soviet attempt at an uncrewed lunar sample return. It was probably similar in design to the Luna 16 spacecraft. It was launched, on a Proton rocket, on October 22, 1969.[3] The engines on the Block D upper stage failed, terminating the mission. This left the spacecraft stranded in Earth orbit. It re-entered within two days.[4]
References
[edit]- ^ "NASA NSSDC Master Catalog - Cosmos 305". Retrieved 25 May 2024.
- ^ a b "Luna Ye-8-5 - Encyclopedia Astronautica". Retrieved 25 May 2024.
- ^ "Luna - Exploring the Moon". orbitalfocus.uk. Retrieved February 23, 2023.
- ^ Siddiqi, Asif A. (2018). "Kosmos 305 [Luna]" (PDF). Beyond Earth: A Chronicle of Deep Space Exploration, 1958-2016. NASA History Program Office: 92. Retrieved February 23, 2023.