Zond 1

Launch Success

Liftoff Time (GMT)

02:42:40

Thursday April 2, 1964

Mission Details

Zond 1

Wiki

Zond 1 was a spacecraft of the Soviet Zond program. It was the second Soviet research spacecraft to reach Venus, although communications had failed by that time. It carried a 90 cm spherical landing capsule, containing experiments for chemical analysis of the atmosphere, gamma-ray measurements of surface rocks, a photometer, temperature and pressure gauges, and a motion/rocking sensor in case it landed in water. At least three previous Soviet planetary probes had been lost due to malfunctions of the ullage rockets (BOZ) on the Blok L stage, but an investigation found that the problem was easily resolved. The spacecraft, a Venera 3MV-1, was launched on April 2, 1964 from Tyuratam and this time the launch vehicle performed flawlessly. During the cruise phase, a slow leak from a cracked sensor window caused the electronics compartment to lose air pressure. This was a serious problem as Soviet electronics relied on vacuum tubes which would overheat without cooling air. An ill-timed command from ground control turned on its radio system while there was still a rarefied atmosphere inside, causing the electronics to short out by corona discharge. Chief Designer Sergei Korolev was upset at the failure of the mission and demanded higher quality control from the OKB-1 Bureau, including X-rays to test for pressure leaks. By mid-April, the electronics in the main spacecraft had completely failed and all signal transmission ceased, but communication via the lander could still be performed, and space radiation and atomic-hydrogen spectrometer measurements were received. The star trackers in the spacecraft were also used to align it for a course-correction burn, but the second one was off by 65 feet per second (20 meters per second). Also one of the star trackers failed, forcing ground controllers to place Zond 1 into a spin-stabilization mode. However, all communications had failed by May 14. It passed 100,000 km from Venus on July 14, 1964.

Heliocentric Orbit

1 Payload

890 kilograms

Rocket

Retired
Molniya

Active 1960 to 1967

RKK Energiya logo

Manufacturer

RKK Energiya

Rocket

Height: 44.23m

Payload to Orbit

LEO: 6,000 kg

GTO: 2,200 kg

Liftoff Thrust

4,378 Kilonewtons

Fairing

Diameter: 2.58m

Height: 6.74m

Stages

4

Strap-ons

4

Launch Site

Site 1/5

Baikonur Cosmodrome, Kazakhstan

Fastest Turnaround

23 hr 32 min

Stats

Molniya


18th

Mission

4th

Mission of 1964

RKK Energiya


82nd

Mission

7th

Mission of 1964

1964


20th

Orbital launch attempt