Rutherford (rocket engine)
Rutherford is a liquid propellant rocket engine, designed in New Zealand by Rocket Lab. It uses LOX and kerosene as propellants and is the first flight-ready engine to use the electric pump feed cycle. It will be used on the company's own rocket, Electron. This is a similar arrangement to the Falcon 9, using nine identical engines on the first stage and one, optimized for vacuum with a longer nozzle, on the second stage. It produces 22,000 N (5,000 lbf) and has a specific impulse of 327 s (3.21 km/s). It was qualified for flight on March, 2016 and is expected to debut in early 2017.
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Rutherford (rocket engine)
Rutherford is a liquid propellant rocket engine, designed in New Zealand by Rocket Lab. It uses LOX and kerosene as propellants and is the first flight-ready engine to use the electric pump feed cycle. It will be used on the company's own rocket, Electron. This is a similar arrangement to the Falcon 9, using nine identical engines on the first stage and one, optimized for vacuum with a longer nozzle, on the second stage. It produces 22,000 N (5,000 lbf) and has a specific impulse of 327 s (3.21 km/s). It was qualified for flight on March, 2016 and is expected to debut in early 2017.
has abstract
Rutherford is a liquid propell ...... pected to debut in early 2017.
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Wikipage page ID
51,666,499
Wikipage revision ID
741,589,673
associated
Caption
First stage Rutherford engine
combustion chamber
country of Origin
designer
fuel
name
Rutherford Vacuum
oxidiser
purpose
First and second stage engine
status
Certified for flight
subject
comment
Rutherford is a liquid propell ...... pected to debut in early 2017.
@en
label
Rutherford (rocket engine)
@en