XRS-2200

The Rocketdyne XRS-2200 was an experimental linear aerospike engine developed in the mid-1990s for the Lockheed Martin X-33 program. The XRS-2200 engine's powerpack was derived from the Rocketdyne J-2 engine, the upper stage engine of the Saturn V moon rocket developed under the Apollo Program in the 1960's. The XRS-2200 used the J-2's combustion cycle and propellant choice.

MainWikipediaGalleryBibliographyTableSearch

Wikimedia, Wikidata
Rocketdyne XRS-2200
aerospike engine, 
United States, aerospike engine, Dong Fang Hong 2, Ekran, 

​

Location: KML, Cluster Map, Maps,

Frameless

Twin Linear Aerospike XRS-2200 Engine

Twin Linear Aerospike XRS-2200 Engine PLW edit

Twin Linear Aerospike XRS-2200 Engine edit

Type	Subtype	Date	Description	Notes	Source
commons	image		Twin Linear Aerospike XRS-2200 Engine		Commons
commons	image		Twin Linear Aerospike XRS-2200 Engine PLW edit		Commons
commons	image		Twin Linear Aerospike XRS-2200 Engine edit		Commons