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| title | chunk | source | category | tags | date_saved | instance |
|---|---|---|---|---|---|---|
| Space Race | 10/18 | https://en.wikipedia.org/wiki/Space_Race | reference | science, encyclopedia | 2026-05-05T13:12:13.188868+00:00 | kb-cron |
Though delayed a year to reach its first flight, Gemini was able to take advantage of the USSR's two-year hiatus after Voskhod, which enabled the US to catch up and surpass the previous Soviet superiority in piloted spaceflight. Gemini had ten crewed missions between March 1965 and November 1966: Gemini 3, Gemini 4, Gemini 5, Gemini 6A, Gemini 7, Gemini 8, Gemini 9A, Gemini 10, Gemini 11, and Gemini 12; and accomplished the following:
Every mission demonstrated the ability to adjust the crafts' inclination and apsis without issue. Gemini 5 demonstrated eight-day endurance, long enough for a round trip to the Moon. Gemini 7 demonstrated a fourteen-day endurance flight. Gemini 6A demonstrated rendezvous and station-keeping with Gemini 7 for three consecutive orbits at distances as close as 1 foot (0.30 m). Gemini 9A also achieved rendezvous with an Agena Target Vehicle (ATV). Rendezvous and docking with the ATV was achieved on Gemini 8, 10, 11, and 12. Gemini 11 achieved the first direct-ascent rendezvous with its Agena target on the first orbit. Extravehicular activity (EVA) was perfected through increasing practice on Gemini 4, 9A, 10, 11, and 12. On Gemini 12, Edwin "Buzz" Aldrin spent over five hours working comfortably during three (EVA) sessions, finally proving that humans could perform productive tasks outside their spacecraft. Gemini 10, 11, and 12 used the ATV's engine to make large changes in its orbit while docked. Gemini 11 used the Agena's rocket to achieve a crewed Earth orbit record apogee of 742 nautical miles (1,374 km). Gemini 8 experienced the first in-space mission abort on March 17, 1966, just after achieving the world's first docking, when a stuck or shorted thruster sent the craft into an uncontrolled spin. Command pilot Neil Armstrong was able to shut off the stuck thruster and stop the spin by using the re-entry control system. He and his crewmate David Scott landed and were recovered safely. Most of the novice pilots on the early missions would command the later missions. In this way, Project Gemini built up spaceflight experience for the pool of astronauts for the Apollo lunar missions. With the completion of Gemini, the US had demonstrated many of the key technologies necessary to make Kennedy's goal of landing a man on the Moon, namely crewed spacecraft docking, with the exception of developing a large enough launch vehicle.
=== Soviet crewed Moon programs ===
Korolev's design bureau produced two prospectuses for circumlunar spaceflight (March 1962 and May 1963), the main spacecraft for which were early versions of his Soyuz design. At the same time, another bureau, OKB-52, headed by Vladimir Chelomey, was developing the LK-1 lunar flyby spacecraft, which would be launched by Chelomey's Proton UR-500 rocket. The Soviet government rejected Korolev's proposals, opting to support Chelomey's project, who gained favor with Khrushchev by employing his son. Officially, the Soviet lunar program was established on August 3, 1964, with the adoption of Soviet Communist Party Central Committee Command 655-268 (On Work on the Exploration of the Moon and Mastery of Space). The circumlunar flights were planned to occur in 1967, and the landings to start in 1968, intending to land a person on the Moon before the Apollo flights. Both of the bureaus submitted their projects for a crewed lunar landing. Korolev's lunar landing program was designated N1/L3, for its N1 super rocket and a more advanced Soyuz 7K-L3 spacecraft, also known as the lunar orbital module ("Lunniy Orbitalny Korabl", LOK), with a crew of two. A separate lunar lander ("Lunniy Korabl", LK), would carry a single cosmonaut to the lunar surface. The N1/L3 launch vehicle had three stages to Earth orbit, a fourth stage for Earth departure, and a fifth stage for lunar landing assist. The combined space vehicle was roughly the same height and takeoff mass as the three-stage US Apollo-Saturn V and exceeded its takeoff thrust by 28% (45,400 kN vs. 33,000 kN. The N1/3L was never successfully tested, the first flight suffered a fire in the first-stage Block A due to a loose bolt, leading to a catastrophic explosion 70 seconds into the flight. Further variations of the N1 had similar catastrophic results in testing. If successful, the N1 would have been capable of carrying a 95 metric tons payload into low earth orbit. The Saturn V comparatively used liquid hydrogen fuel in its two upper stages, and carried a 140.6 metric tons payload to orbit, enough for a three-person orbiter and two-person lander. Chelomey's program assumed using a direct ascent lander based on the LK-1, LK-700, which would be launched using his proposed UR-700 rocket. Following Khrushchev's ouster from power, Chelomey lost his support in the Soviet government, and his proposal didn't receive any funding. Additionally, in August 1965, due to Korolev's opposition, work on the LK-1 was suspended, and later stopped completely. As a replacement, the circumlunar mission would use a stripped-down Soyuz 7K-L1 "Zond", while still retaining the Proton UR-500 booster. To fit two crewmembers, the Zond had to omit the Soyuz orbital module, sacrificing equipment for habitable cabin volume.
=== Outer space treaties ===