ORBITDECKMission Intelligence
Vehicles/New Glenn
DevelopmentBlue OriginUnited StatesFirst Launch: 2025-01-16

New Glenn

Heavy-lift reusable orbital launcher featuring a 7-meter payload fairing and ocean landing recovery.

New Glenn is a two-stage heavy-lift orbital launch vehicle developed by Blue Origin. Named in honor of astronaut John Glenn, the rocket features a massive 7-meter diameter payload fairing and a reusable first stage powered by seven BE-4 methane engines, designed for a minimum of 25 missions with downrange ocean landing recovery on a moving autonomous landing vessel.

SpaceStats Reliability & Flight Record

TOTAL LAUNCHES
1
Orbital missions
SUCCESSFUL
1
0 failures
SUCCESS RATE
100.0%
LANDINGS
0
Reusable First Stage
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New Glenn Orbital Rocket Liftoff
Blue OriginFeatured Photography
New Glenn Orbital Rocket Liftoff
U.S. Space Force / Blue Origin

Architecture Analysis & Development Story

Engineering Dossier

History & Development

Announced in 2016, New Glenn represents Blue Origin's entry into high-energy orbital launch markets. The manufacturing complex at Exploration Park in Cape Canaveral produces the 7-meter diameter tanks and composite structures. Its inaugural launch in early 2025 carries the Blue Ring pathfinder and NASA ESCAPADE Mars dual-probe payloads.

Operational Record & Mission Impact

Contracted for major multi-launch commercial constellations including Amazon Project Kuiper, commercial telecommunication satellites, and NASA deep space exploration missions.

Key Engineering Innovations & Design Highlights

Seven BE-4 staged combustion engines producing 17.1 MN (3.85 million lbf) of thrust using clean-burning Methalox.

Large-volume 7-meter payload fairing offering twice the volume of standard 5-meter commercial fairings.

Hydrolox (LOX/LH2) second stage powered by dual BE-3U expander-cycle vacuum engines.

Aerodynamic strakes and actuating fin control surfaces for high dynamic-pressure atmospheric re-entry recovery.

Technical & Propulsion Specifications

Operator: Blue Origin

Vehicle Dimensions & Mass

Overall Height
98 m
Body Diameter
7 m
Gross Lift-off Mass
1,500 t
Stages Count
2
Fairing Diameter
7 m

First Stage Booster

Main Engines
7x BE-4
Propellant
LOX / Liquefied Natural Gas (Methane)
SL Thrust
17,100 kN
Vacuum Isp
339s
Dry Mass
110 t
Recovery Mode
ASDS_DroneShip

Second Stage

Upper Engine
2x BE-3U
LEO Capacity
45 t
GTO Capacity
13.6 t
TLI (Lunar)
8 t
Cost per Launch
$68,000,000
LEO Price / kg
~$1,511 / kg

Launch Complexes & Spaceports Network

1 Active Launch Pads
Launch Complex 36 (LC-36)
Cape Canaveral Space Force Station
Florida, USA
28.471°N, -80.537°E

SpaceStats Launch Manifest & Database

0 mission records cataloged in database

Full Space Calendar

No individual manifest entries logged in database for New Glenn.

Summary stats and flight achievements are detailed in the overview above.