Astronomy:Kankoh-maru

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Short description: Japanese orbital vehicle design
Kankoh-maru
Kankoh-maru spacecraft.jpg
Artist's concept of Kankoh-maru
FunctionCrewed re-usable rocket
Country of originJapan
Size
Height23.5 m (77 ft)[1]
Diameter18 m (59 ft)[1]
Mass550 t (1,210,000 lb)[1]
Stages1
Capacity
Payload to LEO50 t (110,000 lb)[2]
Launch history
StatusProposed[3]
First stage
Thrust6,888,000 N (1,548,000 lbf) [1]
Boosters
Total thrust2,900,000 N (650,000 lbf) [1]

The Kankoh-maru (観光丸, Kankōmaru) is a proposed vertical takeoff and landing (VTVL), single-stage-to-orbit (SSTO), reusable launch system (rocket-powered spacecraft). According to a document from July 1997, it would have been manufactured by Kawasaki Heavy Industries and Mitsubishi Heavy Industries, with its formal name being the Kawasaki S-1.[1]

Overview

The concept was created by the Japanese Rocket Society [ja] in 1993.[3] This development cost was estimated Template:JPYConvert in 1995.[4]

The name Kankō Maru is derived from the first steam-powered vessel in Edo-era Japan.[3]

See also

References

  1. 1.0 1.1 1.2 1.3 1.4 1.5 Anderson, Erik (July 1997). "Kankoh-maru Flight Manual". Space Future. http://www.spacefuture.com/archive/kankoh_maru_flight_manual.shtml. 
  2. "Kankoh Maru". http://www.astronautix.com/k/kankohmaru.html. 
  3. 3.0 3.1 3.2 Isozaki, Kohki; Yonemoto, Koichi; Kitayama, Osamu; Miyahara, Akira; Watanabe, Hiroyuki; Okaya, Shunichi; Ibusuki, Masayuki (1998). "Status Report on Space Tour Vehicle "Kankoh-maru" of Japanese Rocket Society". International Astronautical Federation 1998. https://www.spacefuture.com/archive/status_report_on_space_tour_vehicle_kankoh_maru_of_japanese_rocket_society.shtml. Retrieved January 28, 2023. 
  4. "Error: no |title= specified when using {{Cite web}}" (in ja). uchumaru.com. 2005-04-11. http://www.uchumaru.com/spaceship/kankohmaru.htm. 

External links