Sputnik 2
Sputnik 2 was an uncrewed Soviet spacecraft launched on November 3, 1957, from the Baikonur Cosmodrome, representing the second artificial Earth satellite and the first to transport a living animal, the dog Laika, into orbit.[1][2]
The payload, a cone-shaped capsule approximately 4 meters tall with a base diameter of 2 meters and a mass of 508 kilograms, remained attached to its R-7 booster stage after separation and entered an elliptical orbit with a perigee of 212 kilometers, an apogee of 1,660 kilometers, and an inclination of 65.3 degrees.[1][3][2]
Equipped with instruments to detect cosmic radiation and atmospheric pressure, as well as a rudimentary life-support system providing oxygen, food, and waste management for Laika—a stray dog conditioned for the mission—the satellite transmitted telemetry data for several weeks.[4][2]
Laika survived the launch stresses but perished within five to seven hours due to cabin overheating from a thermal regulation failure, a fact confirmed by declassified Soviet records contradicting earlier official reports of prolonged survival.[5][2]
The mission demonstrated the feasibility of sustaining biological life through launch and into orbital conditions, yielding critical data on space biology despite the absence of re-entry capability, and accelerated international efforts in space exploration.[1][4]
Sputnik 2 orbited Earth until re-entering and disintegrating in the atmosphere on April 14, 1958.[5]
Historical Context
Origins in the Soviet Space Program
The Soviet space program's foundations for artificial satellites originated in the post-World War II era, leveraging captured German V-2 rocket technology and domestic advancements in ballistic missiles, culminating in Sergei Korolev's OKB-1 bureau developing the R-7 Semyorka intercontinental ballistic missile by 1957, which doubled as the launch vehicle for early satellites.[6] A January 30, 1956, decree from the USSR Council of Ministers formalized plans for an Earth satellite during the International Geophysical Year (1957–1958), incorporating tasks such as launching live organisms to study biological effects of spaceflight, building on prior suborbital dog experiments that began with the R-1E rocket in 1951.[7] [6] Initial efforts focused on a complex "Object D" scientific satellite under Mstislav Keldysh's oversight, but persistent delays in its instrumentation pushed Korolev to propose simpler alternatives, leading to the rapid development of Sputnik 1 as a minimal "Prosteishy Sputnik" (PS-1) launched on October 4, 1957.[6] Following Sputnik 1's success, which demonstrated the R-7's orbital capability, Soviet Premier Nikita Khrushchev, seeking to capitalize on the propaganda victory and mark the 40th anniversary of the October Revolution on November 7, 1957, directed Korolev on October 12 to prepare a more substantial follow-up mission using the next available R-7 booster.[7] [2] Korolev, leveraging ongoing biological research at OKB-1's Biology Division under Vladimir Yazdovsky and Vladimir Chernigovsky, advocated for including a canine payload to test life support systems in orbit, drawing from accumulated data on animal physiology in weightlessness and radiation from high-altitude rocket flights.[6] This decision prioritized speed over thorough design review, bypassing standard bureaucratic approvals; the spacecraft evolved from conceptual sketches directly into parallel mockup and flight hardware production within weeks, reflecting the program's shift from missile-centric origins toward ambitious biological experimentation amid Cold War imperatives.[2] The origins underscored the Soviet program's dual civilian-military character, where ICBM infrastructure enabled opportunistic space achievements, but political urgency often overrode technical caution, as evidenced by the compressed timeline that repurposed Sputnik 1's backup components for a heavier, cone-shaped payload section weighing approximately 508 kg.[7] [2] This approach, while advancing biomedical knowledge incrementally from suborbital tests, highlighted resource constraints and the improvised nature of early Soviet orbital efforts, with Korolev's vision for manned flight influencing the inclusion of life-support prototypes despite the absence of reentry capabilities.[6]Decision to Include a Biological Payload
Following the successful launch of Sputnik 1 on October 4, 1957, Soviet Premier Nikita Khrushchev directed the space program to achieve another orbital launch before the November 7 anniversary of the Bolshevik Revolution, aiming to sustain propaganda momentum amid the intensifying Cold War space race.[8] Chief Designer Sergei Korolev, facing tight deadlines and a fueled R-7 Semyorka rocket already at the Baikonur pad, proposed repurposing an existing biological research capsule—originally developed for suborbital dog flights—as the payload for the second satellite.[2] This capsule, designed to monitor physiological responses to spaceflight conditions, was integrated directly with the rocket's upper stage, forgoing a separate reentry vehicle due to time constraints.[8] The inclusion of a live dog as the payload stemmed from an established Soviet biomedical program dating to 1951, which had tested canines on over a dozen suborbital R-1 and R-2 rocket flights to assess tolerance to acceleration, vibration, weightlessness, and radiation—data deemed essential for eventual human missions.[4] Korolev's proposal, approved by the State Commission on October 10, 1957, prioritized demonstrating that a mammal could survive orbital insertion and early flight phases, thereby validating the R-7's habitability for crewed flights.[2] Unlike prior unmanned probes, this biological experiment addressed gaps in understanding prolonged microgravity effects, with telemetry systems tracking heart rate, respiration, and movement via sensors on the animal.[9] Soviet scientists, including Vladimir Yazdovsky, selected dogs for their physiological similarity to humans and ease of training compared to primates, building on physiological data from earlier missions where survival rates improved through cabin pressurization and thermal controls.[4] The rushed timeline precluded recovery mechanisms, rendering the mission one-way, a compromise justified internally as sufficient for proof-of-concept data on launch stresses and orbital onset, though later declassified accounts revealed overheating risks were underestimated.[8] This decision underscored the program's dual scientific and political imperatives, prioritizing rapid achievement over mission longevity.[2]Design and Engineering
Overall Spacecraft Specifications
Sputnik 2 (PS-2) was a cone-shaped spacecraft module with a total mass of 508.3 kg, launched atop the modified R-7 Semyorka rocket's core stage on November 3, 1957.[1][3] The module measured approximately 4 meters in height from base to apex, with a base diameter of 2 meters, constructed primarily from aluminum alloy sheets riveted to a framework of longerons and rings for structural integrity.[10] Unlike Sputnik 1, the PS-2 satellite remained permanently attached to its expended booster stage in orbit, forming a composite object without separation mechanisms, which simplified design but precluded independent maneuvering.[1] The spacecraft's structure comprised three primary stacked sections within the conical envelope: a forward hermetically sealed cabin for the biological payload, derived from suborbital dog-flight capsules and measuring 0.8 meters in length by 0.64 meters in diameter; a central instrumentation bay housing telemetry systems, scientific sensors, and radio transmitters operating at 20 MHz and 40 MHz frequencies; and an aft compartment containing chemical batteries for power supply and basic thermal control elements, including reflective coatings and passive radiators to manage temperatures without active heating or cooling.[10][3] Attitude stabilization relied on the rocket's residual spin imparted during ascent, with no onboard thrusters or reaction wheels, limiting orientation control to passive means.[10] Telemetry antennas consisted of four extendable rods, enabling continuous transmission of data including physiological readings and environmental parameters until battery depletion.[11]| Parameter | Specification |
|---|---|
| Mass | 508.3 kg |
| Height | ~4 m (conical module) |
| Base Diameter | 2 m |
| Payload Cabin | 0.8 m length × 0.64 m diameter |
| Power Source | Chemical batteries |
| Attitude Control | Passive spin stabilization |
| Separation from Booster | None (integrated in orbit) |