Vector-H

Vector-H
Function	Smallsat launcher
Manufacturer	Vector Launch
Country of origin	United States
Cost per launch	3.5-4.5 Million USD
Size
Height	19.5 m (64 ft)
Diameter	1.2 m (3 ft 11 in)
Mass	11,910 kg (26,260 lb)
Stages	2/3
Capacity
Payload to LEO
Mass	290 kg (640 lb)
Payload to SSO
Mass	95 kg (209 lb)
Associated rockets
Family	Vector (rocket family)
Comparable	Electron, Falcon 1, Firefly Alpha, Prime, Miura 5
Launch history
Status	Canceled
Launch sites	Pacific Spaceport Complex – Alaska (planned); Spaceport Camden (planned); Spaceport Florida Launch Complex 46 (planned)
First stage
Diameter	1.2 m (3 ft 11 in)
Powered by	6 x LP-1
Maximum thrust	39,336 lbf (174,980 N)
Propellant	Propylene / LOX
Second stage
Diameter	1.2 m (3 ft 11 in)
Powered by	1 X LP-3
Maximum thrust	1,135 lbf (5,050 N)
Propellant	Propylene / LOX
Third stage
Diameter	1.2 m (3 ft 11 in)
Propellant	Solid fuel
	[edit on Wikidata]

Vector-H (Vector Heavy)^[1] was a planned two-stage or three-stage orbital expendable launch vehicle in development by the American aerospace company Vector Launch to cover the commercial small satellite launch segment (CubeSats). It was planned to be an expanded version of the Vector-R rocket, more than doubling the payload capacity. After Vector Launch ceased operations in December 2019, the future development of the rocket is unofficially canceled.

^ ^a ^b "Archived copy" (PDF). Archived from the original (PDF) on 2018-03-27. Retrieved 2018-03-27.{{cite web}}: CS1 maint: archived copy as title (link)

[vector-launch.com-1] "Archived copy" (PDF). Archived from the original (PDF) on 2018-03-27. Retrieved 2018-03-27.{{cite web}}: CS1 maint: archived copy as title (link)

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