Gemini
In-active Human Rated Capsule Crew Capacity: 2 Diameter: 3.0 m Height: 5.61 m()
April 8, 1964
Human transportation to low Earth orbit.
Flight Life
Between a few hours and multiple days (14 day is the maximum achieved).
Description
The spacecraft was 18 feet 5 inches (5.61 m) long and 10 feet (3.0 m) wide, with a launch weight varying from 7,100 to 8,350 pounds (3,220 to 3,790 kg).
History
The Gemini crew capsule (referred to as the Reentry Module) was essentially an enlarged version of the Mercury capsule. Unlike Mercury, the retrorockets, electrical power, propulsion systems, oxygen, and water were located in a detachable Adapter Module behind the Reentry Module. A major design improvement in Gemini was to locate all internal spacecraft systems in modular components, which could be independently tested and replaced when necessary, without removing or disturbing other already tested components.
Falcon 9
Starlink Group 17-12
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New Shepard
NS-35
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Starlink Group 10-61
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Long March 2C/YZ-1S
SatNet test satellites
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Falcon 9
Starlink Group 17-10
Space Launch Complex 4E - Vandenberg SFB, CA, USAA batch of 24 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Soyuz 2.1b/Fregat
Glonass-K1 No. 18 (Kosmos 2595) & Kosmos 2596
43/3 (43L) - Plesetsk Cosmodrome, Russian FederationGlonass-K1 are the third generation of satellite design for GLONASS satellite navigation system. GLONASS is a Russian space-based navigation system c…
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Nusantara Lima
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Soyuz 2.1a
Progress MS-32 (93P)
31/6 - Baikonur Cosmodrome, Republic of KazakhstanProgress resupply mission to the International Space Station.
Falcon 9
SDA Tranche 1 Transport Layer B
Space Launch Complex 4E - Vandenberg SFB, CA, USATranche 1 Transport Layer B is one of six missions by the United States Space Force Space Development Agency (SDA) for the Proliferated Warfighter Sp…
