The power supply, with a mass of 51 kg,[35] was in the shape of an octahedral nut with the radio transmitter in its hole.[36] It consisted of three silver-zinc batteries, developed at the All-Union Research Institute of Current Sources (VNIIT) under the leadership of N. S. Lidorenko. Two of them powered the radio transmitter and one powered the temperature regulation system.[35] They were expected to fade out in two weeks, but ended up working for 22 days. The power supply was turned on automatically at the moment of the satellite's separation from the second stage of the rocket.[34]
The satellite had a one-watt, 3.5 kg[20] radio transmitting unit inside, developed by V. I. Lappo from NII-885,[34] that worked on two frequencies, 20.005 and 40.002 MHz. Signals on the first frequency were transmitted in 0.3 sec pulses (under normal temperature and pressure conditions on-board), with pauses of the same duration filled by pulses on the second frequency.[37] Analysis of the radio signals was used to gather information about the electron density of the ionosphere. Temperature and pressure were encoded in the duration of radio beeps, which additionally indicated that the satellite had not been punctured by a meteorite. A temperature regulation system contained a fan, a dual thermal switch, and a control thermal switch.[34] If the temperature inside the satellite exceeded 36 °C the fan was turned on and when it fell below 20 °C the fan was turned off by the dual thermal switch.[33] If the temperature exceeded 50 °C or fell below 0 °C, another control thermal switch was activated, changing the duration of the of radio signal pulses.[34] Sputnik 1 was filled with dry nitrogen, pressurized to 1.3 atm.[38] For the pressure control the satellite had a barometric switch, activated when the pressure inside the satellite fell below 0.35 kg/cm² (approx. 0.34 atm), changing the duration of radio signal impulse.[38]
While attached to the rocket, Sputnik 1 was protected by a cone-shaped payload fairing, with a height of 80 cm and an aperture of 48 degrees.[20] The fairing separated from both Sputnik 1 and the rocket at the same time when the satellite was ejected.[34] Tests of the satellite were conducted at OKB-1 under the leadership of O. G. Ivanovsky.[27] Sputnik 1 was launched by an R-7 rocket on October 4, 1957. It burned up upon re-entry on January 4, 1958.


