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Eclipse (rocket)

Spacecraft and Launch Vehicles

Eclipse is a two-stage, partially reusable medium-lift launch vehicle being developed jointly by Firefly Aerospace and Northrop Grumman. It began as Firefly Beta and then the Medium Launch Vehicle, and it was named Eclipse in May 2025, when Northrop Grumman announced a 50 million US dollar investment in the programme. The rocket is intended as a successor to Northrop Grumman Antares and is designed to place about 16,300 kilograms into low Earth orbit. Both stages burn RP-1 and liquid oxygen and are built with a carbon-fibre composite airframe. The first stage uses seven Miranda engines and is designed to be reusable, while the expendable second stage uses a single Vira vacuum engine. The first launches are planned from Launch Pad 0A at the Mid-Atlantic Regional Spaceport at Wallops Island, Virginia, and the maiden flight is expected in 2029.

Facts
Propulsion
RP-1 and liquid oxygen 2
Status
Under development 2
Comparison
Body Style
Launch vehicle 1
Connections

Exemplifies

Space Transport, Modes
Source Eclipse (rocket) (Wikipedia)

Of Make

Source Eclipse (rocket) (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Eclipse (rocket) (Wikipedia)Lead, developers
Quote, Lead, developers
being jointly developed by Firefly Aerospace and Northrop Grumman

Also in Business Atlas: the manufacturer of this subject.

Source Eclipse (rocket) (Wikipedia)Lead, developers
Quote, Lead, developers
being jointly developed by Firefly Aerospace and Northrop Grumman
Sources
1. Flying Magazine: Firefly's Medium Launch Vehicle Has a New Name-And $50M in Fresh Funding
Flying MagazineLead
Quote, Lead
newly named Eclipse medium-lift launch vehicle
View the Source
2. Eclipse (rocket) (Wikipedia)
  • Lead
    is a two-stage, partially reusable medium-lift launch vehicle
  • Lead, status
    Currently, the maiden launch of Eclipse is expected in 2029.
  • Design
    Both stages of Eclipse will use RP-1 and LOX propellant
  • Lead, developers
    being jointly developed by Firefly Aerospace and Northrop Grumman
  • Exemplifies: Space Transport, Lead, launch vehicle
    medium-lift launch vehicle
  • In Group: Orbital Launch Vehicles, Lead, orbital launch
    can launch 16,300 kg (35,900 lb) into low Earth orbit
View the Source
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