Satellite construction project On 17 December 1954, chief Soviet rocket scientist
Sergei Korolev proposed a developmental plan for an artificial satellite to the Minister of the Defense Industry,
Dimitri Ustinov. Korolev forwarded a report by
Mikhail Tikhonravov, with an overview of similar projects abroad. Tikhonravov had emphasised that the launch of an orbital satellite was an inevitable stage in the development of rocket technology. On 29 July 1955, U.S. President
Dwight D. Eisenhower announced through his press secretary that, during the
International Geophysical Year (IGY), the United States would launch an artificial satellite. Four days later,
Leonid Sedov, a leading Soviet physicist, announced that they too would launch an artificial satellite. On 8 August, the
Politburo of the Communist Party of the Soviet Union approved the proposal to create an artificial satellite. On 30 August, Vasily Ryabikov—the head of the State Commission on the
R-7 rocket test launches—held a meeting where Korolev presented calculation data for a spaceflight trajectory to the Moon. They decided to develop a three-stage version of the R-7 rocket for satellite launches.
National Air and Space Museum On 30 January 1956, the
Council of Ministers approved practical work on an artificial Earth-orbiting satellite. This satellite, named
Object D, was planned to be completed in 1957–58; it would have a mass of and would carry of scientific instruments. The first test launch of "Object D" was scheduled for 1957. • The
USSR Academy of Sciences was responsible for the general scientific leadership and the supply of research instruments. • The Ministry of the Defense Industry and its primary design bureau,
OKB-1, were assigned the task of building the satellite. • The Ministry of the Radio technical Industry would develop the control system, radio/technical instruments, and the
telemetry system. • The Ministry of the Ship Building Industry would develop
gyroscope devices. • The Ministry of the Machine Building would develop ground launching, refuelling, and transportation means. • The Ministry of Defense was responsible for conducting launches. Preliminary design work was completed in July 1956 and the scientific tasks to be carried out by the satellite were defined. These included measuring the density of the atmosphere and its
ion composition, the
solar wind,
magnetic fields, and
cosmic rays. These data would be valuable in the creation of future artificial satellites; a system of ground stations was to be developed to collect data transmitted by the satellite, observe the satellite's orbit, and transmit commands to the satellite. Because of the limited time frame, observations were planned for only 7 to 10 days and orbit calculations were not expected to be extremely accurate. By the end of 1956, it became clear that the complexity of the ambitious design meant that 'Object D' could not be launched in time because of difficulties creating scientific instruments and the low
specific impulse produced by the completed R-7 engines (304 seconds instead of the planned 309 to 310 seconds). Consequently, the government rescheduled the launch for April 1958. Fearing the U.S. would launch a satellite before the USSR, OKB-1 suggested the creation and launch of a satellite in April–May 1957, before the IGY began in July 1957. The new satellite would be simple, light (), and easy to construct, forgoing the complex, heavy scientific equipment in favour of a simple radio transmitter. On 15 February 1957 the Council of Ministers of the USSR approved this simple satellite, designated 'Object PS', PS meaning
"prosteishiy sputnik", or "elementary satellite". This version allowed the satellite to be tracked visually by Earth-based observers, and it could transmit tracking signals to ground-based receiving stations. The rocket was the most powerful in the world; it was designed with excess thrust since they were unsure how heavy the hydrogen bomb payload would be. The R-7 was also known by its GRAU (later GURVO, the Russian abbreviation for "Chief Directorate of the Rocket Forces") designation 8K71. At the time, the R-7 was known to NATO sources as the T-3 or M-104, and Type A. Several modifications were made to the R-7 rocket to adapt it to 'Object D', including upgrades to the main engines, the removal of a radio package on the booster, and a new payload fairing that made the booster almost four metres (14 feet) shorter than its ICBM version. Object D would later be launched as
Sputnik 3 after the much lighter 'Object PS' (Sputnik 1) was launched first. The trajectory of the launch vehicle and the satellite were initially calculated using
arithmometers and six-digit trigonometric tables. More complex calculations were carried out on a newly-installed computer at the
Academy of Sciences. The first launch of an R-7 rocket (8K71 No.5L) occurred on 15 May 1957. A fire began in the Blok D
strap-on almost immediately at liftoff, but the booster continued flying until 98 seconds after launch when the strap-on broke away and the vehicle crashed downrange. Three attempts to launch the second rocket (8K71 No.6) were made on 10–11 June, but an assembly defect prevented launch. The unsuccessful launch of the third R-7 rocket (8K71 No.7) took place on 12 July. The launch of the fourth rocket (8K71 No.8), on 21 August at 15:25
Moscow Time, allowing the delay in the rocket's military exploitation to launch the PS-1 and PS-2 satellites. On 22 September a modified R-7 rocket, named
Sputnik and indexed as 8K71PS, arrived at the proving ground and preparations for the launch of PS-1 began. Compared to the military R-7 test vehicles, the mass of 8K71PS was reduced from , its length with PS-1 was and the
thrust at liftoff was .
Observation complex PS-1 was not designed to be controlled; it could only be observed. Initial data at the launch site would be collected at six separate observatories and telegraphed to
NII-4. Located back in Moscow (at
Bolshevo), NII-4 was a scientific research arm of the
Ministry of Defence that was dedicated to missile development. The six observatories were clustered around the launch site, with the closest situated from the launch pad. These tracking stations were located at
Tyuratam,
Sary-Shagan,
Yeniseysk,
Klyuchi,
Yelizovo,
Makat in
Guryev Oblast, and
Ishkup in
Krasnoyarsk Krai. The observatories used a trajectory measurement system called "Tral", developed by
OKB MEI (Moscow Energy Institute), by which they received and monitored data from
transponders mounted on the R-7 rocket's core stage. The data were useful even after the satellite's separation from the second stage of the rocket; Sputnik's location was calculated from data on the location of the second stage, which followed Sputnik at a known distance. Tracking of the booster during launch had to be accomplished through purely passive means, such as visual coverage and radar detection. R-7 test launches demonstrated that the tracking cameras were only good up to an altitude of , but radar could track it for almost . The booster rocket was located and tracked by the British using the
Lovell Telescope at the
Jodrell Bank Observatory, the only telescope in the world able to do so by radar. == Design ==