Kankoh-maru

**Kankoh-maru**
	; Kankoh-maru (Provided by uchumaru.com)
Function	Manned Re-usable rocket
Country of origin	Japan
Size
Height	23.5 m (77 ft)
Diameter	18 m (59 ft)
Mass	550 t (1,210,000 lb)
Stages	1
Capacity
Payload to LEO	4 t (8,800 lb)
Launch history
Status	Proposed

The Kankoh-maru (観光丸, Kankōmaru^?) is the name of a proposed vertical takeoff and landing (VTVL), single-stage-to-orbit (SSTO), reusable launch system (rocket-powered spacecraft).^[1]

Details

The concept was created by the [[{{{1}}}]]^[] in 1993.^[2]^{[need quotation to verify]}

This development cost was estimated ¥2.67 trillion ($28 billion) in 1995.^[2]^{[need quotation to verify]}

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Size
Kankoh-maru (Provided by uchumaru.com)
Function	Manned Re-usable rocket
Country of origin	Japan
Height	23.5 m (77 ft)^[1]
Diameter	18 m (59 ft)^[1]
Mass	550 t (1,210,000 lb)^[1]
Stages	1
Capacity
Payload to LEO	4 t (8,800 lb)^[2]
Launch history
Status	Proposed^[2]