• Overview
  • Characteristics
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Overview

A direct descendent of the rocket engine that powered Apollo to the moon.


Designed specifically to power heavy lift launch vehicles into Earth orbit and then beyond Earth orbit, Pratt & Whitney Rocketdyne's J-2X engine will employ some of the design concepts of its forebearer. It will also use modern analyses, materials and processes that have been proven on today's engine systems for greater efficiencies and increased power.


Total thrust in vacuum will be 294,000 pounds, and specific impulse will be 448 seconds, both significant increases over the original J-2. Each expendable J-2X is capable of four operational starts for 2,000 seconds, and will be able to restart in space in support of missions beyond low-Earth orbit. The engine will use a gas generator power cycle and burn liquid hydrogen with liquid oxygen, both sustained in cryogenic states.


At 15 feet, the J-2X will be four-feet taller than its predecessor and will weigh in at 5,450 pounds.


The first unmanned flight of the J-2X is set for 2014.

 

 

 

 

 

 

 

 

 

 

Characteristics

J-2X Engine

Propellants
Fuel: Hydrogen
Oxidizer: Liquid Oxygen
 
Thrust (in vacuum): 294,000 lbs.
 
Specific Impulse (in vacuum): 448 sec.
 
Pressure-Combustion Chamber: 1,380 psia
 
Mixed Ration (O/F): 5.5-4.5
 
Nozzle Area Ration: 92
 
Weight: 5,450 lb.

Dimensions
Length: 185 in.
Diameter: 120 in.

Contact Information

Sales & Marketing Contact

Customer, industry and partner information
info@pwr.utc.com

 

Media Contact

Carri Karuhn
818-586-4963
carri.karuhn@pwr.utc.com

 

Additional Information

Click here to request additional information about Pratt & Whitney Rocketdyne