Launcher

Tundra

Micro-lift launcher designed around in-house multi-propellant engines.

Launcher Info

Status
Planned
Maximum Performance
Micro-Lift
Type
Rocket Launcher
Reusability

Launcher Cofigurations

Tab 1
Tab 2
Tab 3

Related Links

No items found.

Additional Background

This is NordSpace's first orbital-class vehicle.

Launches From

No items found.

Engines

NordSpace
Prototype Built
Liquid
RP1
Oxygen

Common Payloads

NordSpace
Planned
Constellation

Company

Privately-Held
Active Business

Operated By

No items found.

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Service History

Development History

Engine development and qualification occurred over 2023 and 2024.

Launch Manifest

No items found.

Launch History

No items found.
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Tundra Standard
Initial configuration.
Configuration Service Status
Under Development
Mass to LEO Classification
Micro-Lift
Performance
Orbit
Mass to Orbit (kg)
Low-Earth Orbit (LEO)
500
No Data
Sun-Synchronous Orbit (SSO)
No Data
Geostationary Transfer Orbit (GTO)
No Data
Geostationary Orbit (GSO)
No Data
Lunar Transfer Orbit (LTO)
No Data
Mars Transfer Orbit (MTO)
No Data
Specs
Orbit
Mass to Orbit (kg)
Length
No Data
Diameter
No Data
Dry Mass
No Data
Pressurized Volume
No Data
No detailed launcher stage information is available.