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Hace 3 días · Contents. hide. (Top) North American X-15 Pilots Group (USA) 1958. 1959. 1960. 1962. 1963. 1964. 1965. 1966. 1967. 1968. 1969. 1970. 1971. 1972. 1973. 1974. 1976. 1977. 1978. 1979. 1980. 1982. 1983. 1984. 1985. 1986. 1987. 1988. 1989. 1990. 1992. 1994. 1996. 1997. 1998.
Hace 3 días · The Gemini spacecraft carried a two-astronaut crew. Ten Gemini crews and 16 individual astronauts flew low Earth orbit (LEO) missions during 1965 and 1966. Gemini's objective was the development of space travel techniques to support the Apollo mission to land astronauts on the Moon.
Hace 4 días · Sally Kristen Ride (May 26, 1951 – July 23, 2012) was an American astronaut and physicist. Born in Los Angeles, she joined NASA in 1978, and in 1983 became the first American woman and the third woman to fly in space, after cosmonauts Valentina Tereshkova in 1963 and Svetlana Savitskaya in 1982. She was the youngest American ...
Hace 3 días · During the flight, the spacecraft attained a maximum velocity of 28,075 km/hour and an altitude of 265 km. The capsule reentered under the manual control of the pilot after completing 22 orbits, landing about 130 km southeast of Midway Island in the Pacific Ocean, about 6.4 km from the prime recovery ship, USS Kearsarge.
Hace 1 día · Ed Dwight could have been the only black astronaut in the 1960s – but politics got in the way. In 2024, at the age of 90, he finally got his chance to go into orbit.
Hace 4 días · The CM separated from the SM at 16:21:13 UT on 24 July. Apollo 11 splashed down in the Pacific Ocean on 24 July 1969 at 16:50:35 UT (12:50:35 p.m. EDT) after a mission elapsed time of 195 hrs, 18 mins, 35 secs. The splashdown point was 13 deg 19 min N, 169 deg 9 min W, 400 miles SSW of Wake Island and 24 km (15 mi) from the recovery ship USS ...
Hace 5 días · Lunar Module Spacecraft and Subsystems. The lunar module was a two-stage vehicle designed for space operations near and on the Moon. The spacecraft mass of 16456 kg was the total mass of the LM ascent and descent stages including propellants (fuel and oxidizer). The dry mass of the ascent stage was 2260 kg and it held 2387 kg of propellant.
