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Luna E-1
Luna 1 / E-1
Luna 1 / E-1
Credit: NASA
Russian lunar impact probe. The first spacecraft to achieve escape velocity and the first to reach the Moon. The spacecraft was sphere-shaped. Five antennae extended from one hemisphere.

AKA: E-1. Status: Operational 1958. First Launch: 1958-09-23. Last Launch: 1959-01-02. Number: 4 . Gross mass: 361 kg (795 lb).

Instrument ports also protruded from the surface of the sphere. There were no propulsion systems on the spacecraft itself. The spacecraft also included various metallic emblems with the Soviet coat of arms.

At a distance of 113,000 km from Earth, a large (1 kg) cloud of sodium gas was released by the spacecraft. This glowing orange trail of gas, with the brightness of a sixth-magnitude star, allowed astronomers to track the spacecraft. It also served as an experiment on the behavior of gas in outer space. The spacecraft contained radio equipment, a tracking transmitter, and telemetering system, five different sets of scientific devices for studying interplanetary space, including a magnetometer, Geiger counter, scintillation counter, and micrometeorite detector, and other equipment. The measurements obtained during the missions provided new data on the Earth's radiation belt and outer space, including the discovery that the Moon had no magnetic field and that a solar wind, a strong flow of ionized plasma emanating from the Sun, streamed through interplanetary space.


More at: Luna E-1.

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Luna E-1A Russian lunar impact probe. First probe to impact lunar surface. Delivered a pennant to the surface of the Moon and conducted research during flight to the Moon.

Family: Lunar Crashers, Moon. Country: Russia. Launch Vehicles: R-7, Vostok-L 8K72. Projects: Luna. Launch Sites: Baikonur, Baikonur LC1. Agency: Korolev bureau. Bibliography: 175, 2, 296, 474, 6, 12770.
Photo Gallery

Luna 1Luna 1
Credit: Manufacturer Image



1958 March 20 - . LV Family: R-7. Launch Vehicle: Vostok-L 8K72.
1958 September 2 - . LV Family: R-7. Launch Vehicle: Vostok-L 8K72.
1958 September 23 - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Vostok-L 8K72. FAILURE: Launcher disintegrated 93 seconds after launch due to longitudinal resonance of strap-ons.. Failed Stage: 0.
1958 October 11 - . 08:42 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Vostok-L 8K72. FAILURE: Launcher disintegrated 104 seconds after launch due to longitudinal resonance of strap-ons.. Failed Stage: 0.
1958 December 4 - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Vostok-L 8K72. FAILURE: Core engines shut off at 245 seconds into the flight. Cause was a loss of lubrication to the hydrogen peroxide pump.. Failed Stage: 1.
1959 January 2 - . 16:41 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Vostok-L 8K72. FAILURE: Failure of the launch vehicle control system.. Failed Stage: G.
1959 June 18 - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Vostok-L 8K72. FAILURE: Inertial system failed at 153 seconds after launch. Vehicle destroyed by range safety.. Failed Stage: G.
1959 September 12 - . 06:39 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Vostok-L 8K72.

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