The information provided below is based on Rocket Lab Electron space vehicles.
Flight profile
The Electron space vehicle consists of three stages. The first stage provides most of the thrust to leave Earth’s atmosphere and separates from the rest of the space vehicle (including the payload) once it reaches a certain altitude. This falls back to Earth and lands in the EEZ. These can be (and previously have been) recovered for reuse. Some overseas operators are researching, developing and using self-recovering launch vehicles, but this technology is not yet in use in New Zealand.
The second stage carries the payload to a near-orbital trajectory. The third stage provides final orbital insertion and deployment of the payload.
Vehicle parts
The space vehicle has four parts: stage 1, stage 2, kick stage and fairing.
- Stage 1 is made of nine Rutherford engines, bulkhead tanks for propulsion and pneumatics materials, and an interstage.
- Stage 2 comprises a single engine, high-voltage batteries and a bulkhead tank for propulsion materials.
- Kick stage is a single Curie engine and propellant tanks, and carries the payload to orbit.
- Fairing is a shell that surrounds the kick stage and payload, protecting them from the hazards of launch.
Carbon fibre composite
The structural material of the launch vehicle is carbon fibre reinforced polymer. The carbon filaments are chemically inert and do not react to seawater.
Propellants
Liquid oxygen and RP-1 kerosene (a rocket propellant version of kerosene) are used on both the first and second stages of the launch vehicle. Liquid oxygen, if released to the atmosphere, rapidly boils and returns to the atmosphere as gaseous oxygen. RP-1 kerosene is a highly refined grade of hydrocarbon with low density, film and rapid evaporation.
Pneumatics
All inflight pneumatic systems use stored pressurised cold gases to provide tank pressurisation, for cold-gas manoeuvring thrust in space, and for stage separation mechanisms.
Engines
The launch vehicle uses nine engines for stage 1, a single Rutherford engine for stage 2 and a single Curie engine for the kick stage. The engines are constructed of Inconel, an inert nickel alloy. Each engine is mounted to the thrust section of the launch vehicle.
Batteries
The launch vehicle carries 13 high-powered lithium batteries for stage 1, mounted at the rear of the launch vehicle with the engines. Stage 2 carries three batteries, two of which are jettisoned as they become exhausted during flight. The remaining battery is carried with the second stage into orbit and continues to power the stage 2 engine.
The stage 1 batteries remain with the stage 1 structure as it lands in the EEZ. The stage 2 batteries will burn up entirely. The batteries are lithium-based and contain no lead, acid, mercury, cadmium, or other toxic heavy metals.