FG-46

The FG-46 is a Chinese spin stabilized solid rocket motor burning HTPB-based composite propellant. It was developed by China Hexi Chemical and Machinery Corporation for use in the Long March 2E on GTO missions. It first flew as a prototype SPTS-M14 on July 16, 1990 on the Badr A mission. It had its first commercial mission orbiting the AsiaSat 2 on November 28, 1995 and exactly one month later, on December 28 its second and last mission for EchoStar 1.

MainWikipediaGalleryBibliographyTableSearch

1995  Wikidata
length 2936 millimetre, diameter 1700 millimetre, mass 557 kilogram, 
perigee kick motor, solid-propellant rocket, 
Reman, 1990s, Republic of Haiti, 1995, perigee kick motor, Ekran, Dong Fang Hong 2, Tarshish, Sikh Confederacy, Ashkenaz, Persia, China, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, 

​

Location: KML, Cluster Map, Maps,

Frameless

Type	Subtype	Date	Description	Notes	Source