cosmos.wikisort.org - Spacecraft

Kosmos 379 (Russian: Космос 379 meaning "Cosmos 379") was an unmanned test of the LK (the Soviet counterpart of the Apollo Lunar Module) in Earth orbit.

Kosmos 379

A standard LK
Operator	Soviet Union
COSPAR ID	1970-099A
SATCAT no.	04760
Spacecraft properties
Spacecraft type	T2K
Launch mass	7,495 kilograms (16,524 lb)
Start of mission
Launch date	24 November 1970, 11:00:00 (1970-11-24UTC11Z) UTC
Rocket	Soyuz-L
Launch site	Baikonur 31/6
Orbital parameters
Reference system	Geocentric
Regime	Low Earth
Eccentricity	0.004161
Perigee altitude	198 kilometres (123 mi)
Apogee altitude	253 kilometres (157 mi)
Inclination	51.6 degrees
Period	88.7 m

Mission

Earth orbit simulated propulsion system operations of a nominal lunar landing mission. Kosmos 379 entered a 192 to 232 km low Earth orbit. After three days it fired its motor to simulate hover and touchdown on the moon, in imitation of a descent to the lunar surface after separation of the Blok D lunar crasher propulsion module. The engine firing changed its orbit from 192 km X 233 km to 196 km X 1206 km (delta-V = 263 m/s).

After a simulated stay on the Moon, it increased its speed by 1.518 km/s, simulating ascent to lunar orbit making the final apogee 14,035 km. These main maneuvers were followed by a series of small adjustments simulating rendezvous and docking with the Soyuz 7K-L3. The LK lander tested out without major problems and decayed from orbit on September 21, 1983.[1]

Parameters

• Spacecraft: T2K
• Mass: 5500 kg
• Crew: None
• Launched: November 24, 1970
• Landed: Reentered September 21, 1983
• Orbit: 192 km

References

External links

• Mir Hardware Heritage
  • Mir Hardware Heritage - NASA report (PDF format)
  • Mir Hardware Heritage (wikisource)

На других языках

---

- [en] Kosmos 379

---

[ru] Космос-379

Космос-379 (Т2К231) — космический аппарат предназначенный для отработки систем советского лунного корабля ЛК в рамках лунной программы.[2]

---

---