Launch Success
Liftoff Time (GMT)
12:57:00
Wednesday July 6, 1966
Last launch of the first Proton version.
Proton 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.
Low Earth Orbit
1 Payload
8,300 kilograms
Manufacturer
KhrunichevRocket
Height: 39.8m
Payload to Orbit
LEO: 12,200 kg
GTO: 0 kg
Liftoff Thrust
8,387 Kilonewtons
Fairing
Diameter: 4.15m
Height: 8.5m
Stages
2
4th
Mission
2nd
Mission of 1966
195th
Mission
30th
Mission of 1966
67th
Orbital launch attempt