NEXT SPACEFLIGHT

Status

Failure

N-4 n°3

Launch Time
Thu Mar 24, 1966 14:39 UTC

The interstage of the launcher was damaged, and the engine of the second stage exploded.

Rocket

Proton
RVSN USSR
Status: Retired
Liftoff Thrust: 8,387 kN
Payload to LEO: 12,200 kg
Payload to GTO: 0 kg
Stages: 2
Strap-ons: 0
Rocket Height: 39.8 m
Fairing Diameter: 4.15 m
Fairing Height: 8.5 m

Mission Details

N-4 n°3

N-4 n°3 is a satellite of the N-4 constellation. The N-4 heavy science satellites were developed by Vladimir Chelomei's OKB-52 in the early 1960s. Baptized "Proton", they will give this name to the UR-500 launcher which will put them into orbit.

They are designed to study very high-energy particles in low Earth orbit, assess the hazard they represent, and determine the intensity and energy spectrum of electrons and gamma rays. These studies are not possible on Earth, because the charged particles are mainly absorbed by the atmosphere.

They are sized to operate in orbit for forty-five days, and are equipped with four solar panels, several batteries and a thermoregulation system. The batteries are located in small capsules placed between the central body and the external envelope of the satellite.

The satellite was destroyed in the atmosphere because of the failure of the launch.

Payloads: 1
Total Mass: 8,300.0 kg
Low Earth Orbit

Location

Site 81/24, Baikonur Cosmodrome, Kazakhstan

Stats

1966

26th orbital launch attempt

Proton

3rd mission
1st mission of 1966
1st failed mission