Launcher

Gravity-1

Solid-fuel multiple booster configuration in a relatively-unique configuration around a central core. Includes three stages in the primary booster core, and four solid-fueled boosters.

Launcher Info

Status
In Service
Maximum Performance
Medium-Lift
Type
Rocket Launcher
Reusability

Launcher Cofigurations

Tab 1
Tab 2
Tab 3

Related Links

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Additional Background

An entirely solid-fueled design, it can be augmented with a liquid-fueled third stage according to product literature. Designed to deliver 4 tons of payload to Sun-Synchronous Orbit, or 6.5 tons to Low Earth Orbit.

First launch in January 2024 was successful.

Launches From

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Engines

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Common Payloads

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Company

Privately-Held
Active Business

Operated By

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Service History

Development History

Launch Manifest

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Launch History

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Gravity-1 Standard
Standard launcher configuration.
Configuration Service Status
In Service
Mass to LEO Classification
Medium-Lift
Performance
Orbit
Mass to Orbit (kg)
Low-Earth Orbit (LEO)
6350
No Data
Sun-Synchronous Orbit (SSO)
4218
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
30
No Data
Diameter
30
No Data
Dry Mass
No Data
Pressurized Volume
No Data
No detailed launcher stage information is available.