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 17-1
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.
Falcon 9
Starlink Group 12-22
Space Launch Complex 40 - Cape Canaveral SFS, FL, USAA batch of 23 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Falcon 9
Starlink Group 11-16
Space Launch Complex 4E - Vandenberg SFB, CA, USAA batch of 27 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Soyuz 2.1b/Fregat-M
Kosmos 2588
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Kinetica 1
6 satellites
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Falcon 9
Starlink Group 12-15
Space Launch Complex 40 - Cape Canaveral SFS, FL, USAA batch of 23 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Long March 7A
ChinaSat 3B
201 - Wenchang Space Launch Site, People's Republic of ChinaChinese communication geostationary satellite for unknown purposes.
Ceres-1S
Tianqi 16-18 & 20
Oriental Spaceport mobile launch ship - Sea Launch4 small satellites for LEO Internet of Things (IoT) communication purposes.
PSLV-XL
EOS-09 (RISAT-1B)
Satish Dhawan Space Centre First Launch Pad - Satish Dhawan Space Centre, IndiaRISAT-1B is the third in the series of radar imaging RISAT-1 satellites of ISRO using an active C-band SAR (Synthetic Aperture Radar), providing all-…
Electron
The Sea God Sees (iQPS Launch 2)
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