Soyuz 7K-L1E
Spacecraft · Russia
Original archive entry. The text, images and links below are kept as they were written.
Credit: RKK Energia
Russian manned lunar orbiter. Modification of Soyuz circumlunar configuration used in propulsion tests of the Block D stage. Technology satellite, Russia. Launched 1969 - 1970. Used the Blok-D bus.
The L1E provided guidance to the Block D and was equipped with television cameras that viewed the behavior of the Block D stage propellants under zero-G conditions. Probably included a dummy descent module (not recovered).
More at: Soyuz 7K-L1E.
Related
- Family
- Lunar Orbiters, Moon
- Country
- Russia
- Engines
- KTDU-53
- Launch Vehicles
- Proton, Proton-K/D
- Launch Sites
- Baikonur, Baikonur LC81/23
- Agency
- Korolev bureau, MOM
Photo Gallery
Zond
Credit: Manufacturer Image
Chronology
3 events
1969 January 24
- Mishin's lunar plans - . Related Persons: Mishin. Spacecraft: Soyuz 7K-L1E, LK, LKR, , Luna Ye-8. Mishin notes that: 1. T1K, T2K, L1E are essential. 2. One more time reviewed the scheme for a lunar expedition of LK + LK-R + Ye-8. (Mishin Diaries 2-158).
1969 November 28
09:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/D. FAILURE: First stage malfunction.. Failed Stage: 1.- Soyuz 7K-L1E s/n 1 - first stage malfunction - .
Payload: Soyuz 7K-L1E s/n 1. Mass: 10,380 kg (22,880 lb). Nation: Russia.
Agency: RVSN.
Program: Luna.
Class: Moon.
Type: Manned lunar spacecraft. Spacecraft Bus: Block D.
Spacecraft: Soyuz 7K-L1E.
Decay Date: 1969-11-16 .
Attempted test flight of Block D upper stage in N1 lunar crasher configuration. Payload was a modified Soyuz 7K-L1 circumlunar spacecraft, which provided guidance to the Block D and was equipped with television cameras that viewed the behavior of the Block D stage propellants under zero-G conditions. Mission flown successfully over a year later as Cosmos 382.
1970 December 2
17:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/D.- Cosmos 382 - .
Payload: Soyuz 7K-L1E s/n 2K. Mass: 10,380 kg (22,880 lb). Nation: Russia.
Agency: MOM.
Program: Lunar L3.
Class: Manned.
Type: Manned spacecraft. Spacecraft Bus: Block D.
Spacecraft: Soyuz 7K-L1E.
Duration: 8,549.30 days. USAF Sat Cat: 4786 . COSPAR: 1970-103A. Apogee: 5,269 km (3,273 mi). Perigee: 2,384 km (1,481 mi). Inclination: 55.90 deg. Period: 171.00 min.
Test of Block D upper stage in its N1 lunar crasher configuration in earth orbit. The three maneuvers simulated the lunar orbit insertion burn; the lunar orbit circularization burn; and the descent burn to bring the LK lunar lander just over the surface. Payload was a modified Soyuz 7K-L1 circumlunar spacecraft, which provided guidance to the Block D and was equipped with television cameras that viewed the behavior of the Block D stage propellants under zero-G conditions.
Maneuver Summary:
190km X 300km orbit to 303km X 5038km orbit. Delta V: 982 m/s
318km X 5040km orbit to 1616km X 5071km orbit. Delta V: 285 m/s
1616km X 5071km orbit to 2577km X 5082km orbit. Delta V: 1311 m/s
Total Delta V: 2578 m/s.
