There is 1 images added on 12 October 2018
Raptor  
Initial Operational Capability (IOC): 2020
Total Production: ?
Origin: United States of America
Corporations: SpaceX
Parent System: Raptor
Initial Operational Capability (IOC): 2020
Total Production: ?
Reviews
There are no reviews so far

Description: The Raptor is a space rocket engine developed by SpaceX to support the United States Air Force (USAF) Evolved Expandable Launch Vehicle (EELV) program and future flights to Mars powering new space launch systems. The USAF awarded a $33.6 million contract for Raptor engine development in January 2016. The Raptor rocket engine burns a mixture of liquid methane and liquid oxygen to provide a maximum thrust at liftoff of 448,000 pounds far exceeding Merlin 1D engine performance. The new engine development is expected to run in the 2010s and possible early 2020s when should deliver a functional engine.

Raptor Specifications

Weight
Thrust: 448,000 pound (203 ton)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Operators & Related Equipment


OperatorsItems

Grand Total ?1
 
Copyright © 2003-2018 deagel.com website. All rights reserved.
This website has been optimized for HTML 5 and CSS 3.