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Ātea-2

Rocket Lab has also developed a design for a larger sub-orbital vehicle, capable of carrying payloads of up to 70kg to space. Peak altitude for a nominal payload mass of 25kg is approximately 250km.

Atea 2 New ZealandĀtea-2 is designed purely as a vehicle to conduct scientific research. Its design ethos enables it to undertake a variety of mission profiles with minimal reconfiguration. The vehicle can be clustered to provide large launch payload weights and shortened if lower altitudes or payload weights are desired.

The principle is to have a completely flexible vehicle that can be configured easily to differing launch profiles.

View further technical specifications for Atea-2.

 

Parameter Performance
Maximum Altitude Up to 250 km
Maximum Diameter 250 mm
Length 6000 mm
Launch Weight (wet) > 250 kg
Max. Payload Weight 70 kg
Max. Launch G-Force 16 g’s
Max. Velocity > Mach 4
Standard Payload Size Ø 250mm x 2000mm L


Environmental Considerations

Ātea-2 Rocket Vs Car C02 Output - An average car produces approximately 2,000 kg of C02 per year, (based on 5,000 miles of travelling). A single Ātea rocket produces 14 kg of C02 per launch - roughly equivalent to running one car for three days.

Animation

View the animation below for an artistic rendering of the flight profile.

Post Your Comment at YouTube.

Related Links

Contact Rocket Lab for payload enquiries, read more about Ātea-1 or return to Rocket Lab Programs.