Function | Small satellite launch vehicle |
---|---|
Manufacturer | Vector Launch |
Country of origin | United States |
Cost per launch | 2–3 million USD |
Size | |
Height | 12 m |
Diameter | 1.2 m |
Mass | 5,000 kg |
Stages | 2/3 |
Capacity | |
Payload to LEO | |
Mass | 60 kg [1] |
Payload to SSO | |
Mass | 26 kg [2] |
Associated rockets | |
Family | Vector (rocket family) |
Derivative work | Vector-H |
Comparable | Electron, Falcon 1, Firefly Alpha |
Launch history | |
Status | Active |
Launch sites | Mojave Air and Space Port Spaceport Camden Pacific Spaceport Complex – Alaska (planned) MARS Pad OB (planned) Spaceport Florida Launch Complex 46 (planned) |
Total launches | 2 |
Success(es) | 2 |
Failure(s) | 0 |
First stage | |
Diameter | 1.2 m (3 ft 11 in) |
Powered by | 3 X Hadley |
Maximum thrust | 15,000 lbf (67,000 N) |
Propellant | Kerosene / LOX |
Second stage | |
Diameter | .635 m (2 ft 1.0 in) |
Powered by | 1 X LP-2 |
Maximum thrust | 1,000 lbf (4,400 N) |
Burn time | 433 seconds |
Propellant | Propylene / LOX |
Vector-R (Vector Rapid) is a two-stage orbital expendable launch vehicle under development by the American aerospace company Vector Launch to cover the commercial small satellite launch segment (CubeSats).[3] Vector Launch went bankrupt in December 2019 and re-emerged in October 2020.[4] Two prototypes were launched in 2017.
The rocket completed a maiden test flight at low altitude in May 2017.[5] Vector Launch was planning the maiden orbital launch from the Pacific Spaceport Complex in Alaska in 2019,[6] but paused operation in August 2019 due to an uncertain financing situation.[7]
An upgraded version of the Vector-R, called the Vector-H (Heavy), is in development as well.