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Soviet and Russian Lunar Exploration

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was difficult to escape in the ocean <strong>and</strong> could take some time to find. They also argued<br />

against the expense involved in having a big recovery fleet at sea.<br />

The timing for <strong>Russian</strong> around-the-moon missions around the sun-Earth-moon<br />

symmetries was therefore quite complex [14]. To meet all these requirements, there are<br />

only about six launching windows, each about three days long <strong>and</strong> a month apart,<br />

each year. There can be long periods when there are no optimum conditions. There<br />

were no optimum launch windows for Zond to the moon between January <strong>and</strong> July<br />

1969, the climax of the moon race. The scarcity of these opportunities explains why<br />

several L-1s (e.g., Zond 4) were fired away from the moon. Although these missions<br />

caused mystery in the West, the primary <strong>Russian</strong> interest was in testing navigation,<br />

tracking <strong>and</strong> the reentry corridor. Having the moon in the sky was not absolutely<br />

necessary for these things <strong>and</strong> since it was not available anyway, they flew these<br />

missions without going around the moon.<br />

L-l/Zond<br />

Length<br />

Diameter<br />

Span<br />

Weight<br />

Habitable volume<br />

Engine<br />

Fuel<br />

Thrust<br />

Specific impulse<br />

5m<br />

2.7 m (base)<br />

9m<br />

5,680 kg<br />

3.5m 3<br />

One KDU-35<br />

AK27 <strong>and</strong> hydrazine<br />

425 kg<br />

276 sec<br />

Block D<br />

Weight 13,360 kg<br />

Fuel Oxygen <strong>and</strong> kerosene<br />

Thrust 8,500 kg<br />

Specific impulse 346<br />

Length 5.5 m<br />

Diameter 3.7 m<br />

Source: Portree (1995); RKK Energiya (2001)<br />

When the L-1 Zond was wheeled out for its first test - Cosmos 146, set for 10th March<br />

1967 - the three-stage UR-500K Proton stood over 44 m tall <strong>and</strong> must have been a<br />

striking sight. The first two tests were called the L-1P, P for 'preliminary' indicating<br />

that a full version of Zond would not be used <strong>and</strong> that a recovery would not be<br />

attempted. The first stage would burn for 2 min with 894 tonnes of thrust. The second<br />

stage would burn for 215 sec. The third stage would place Zond or the L-1 in low-<br />

Earth orbit in a 250 sec burn. Finally, the Korolev block D fourth stage would fire<br />

100 sec to achieve full orbit. One day after liftoff, the fourth stage, block D, would<br />

relight on the first northbound pass over the equator to send Zond out to a simulated<br />

moon [15].

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