About: FG-46

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The FG-46 (a.k.a. EPKM and SpaB-170) is a Chinese spin stabilized solid rocket motor burning HTPB. It was developed by (also known as the 6th Academy of CASIC) for use in the Long March 2E on GTO missions. It first flew as a prototype SPTS-M14 on July 16, 1990 on the 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 .

Attributes	Values
rdf:type	television show
rdfs:label	FG-46 (en) FG-46 (in)
rdfs:comment	FG-46 (AKA EPKM dan SPAB-170) adalah motor roket spin padat stabil Cina berbahan bakar HTPB. Roket ini dikembangkan oleh China Hexi Chemical and Machinery Corporation (juga dikenal sebagai Akademi 6 dari CASIC) untuk digunakan dalam Long March 2E di misi GTO. Roket ini pertama terbang sebagai prototipe PKM pada tanggal 16 Juli 1990 pada misi Badr A. Itu misi komersial pertama yang mengorbit AsiaSat 2 pada tanggal 28 November 1995 dan tepat satu bulan kemudian, pada tanggal 28 Desember misi kedua dan terakhir untuk EchoStar 1. (in) The FG-46 (a.k.a. EPKM and SpaB-170) is a Chinese spin stabilized solid rocket motor burning HTPB. It was developed by (also known as the 6th Academy of CASIC) for use in the Long March 2E on GTO missions. It first flew as a prototype SPTS-M14 on July 16, 1990 on the 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 . (en)
name	FG-46 (en)
dcterms:subject	Solid-fuel rockets Rocket engines of China
Wikipage page ID	47336979 (xsd:integer)
Wikipage revision ID	1084019220 (xsd:integer)
Link from a Wikipage to another Wikipage	Revolutions per minute Geostationary transfer orbit Government of China Long March 2E Solid-fuel rocket Hydroxyl-terminated polybutadiene AsiaSat 2 Solid-fuel rockets China China Aerospace Science and Industry Corporation Rocket engines of China Fiberglass Specific impulse Spin-stabilisation Rocket engine dbr:China_Hexi_Chemical_and_Machinery_Corporation dbr:EchoStar_1 dbr:Badr_A
sameAs	FG-46 FG-46 FG-46 FG-46
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_rocket_engine dbt:Reflist dbt:Rocket-stub dbt:Rocket_engines
country of origin	China
designer	dbr:China_Hexi_Chemical_and_Machinery_Corporation
first date	1995-11-28 (xsd:date)
fuel	Hydroxyl-terminated polybutadiene
purpose	Kick engine (en)
status	Out of Production (en)
type	solid (en)
used in	0001-03-02 (xsd:gMonthDay)
has abstract	The FG-46 (a.k.a. EPKM and SpaB-170) is a Chinese spin stabilized solid rocket motor burning HTPB. It was developed by (also known as the 6th Academy of CASIC) for use in the Long March 2E on GTO missions. It first flew as a prototype SPTS-M14 on July 16, 1990 on the 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 . It has a total nominal mass of 6,001 kg (13,230 lb), of which 5,444 kg (12,002 lb) is propellant load and its burn out mass is 529 kg (1,166 lb). It has an average thrust of 190 kN (43,000 lbf) with a specific impulse of 292 seconds burning for 87 seconds, with a total impulse of 1.589 MN (357,000 lbf). It is spin stabilized at 40 rpm and the propellant mass can be reduced by up to 350 kg (770 lb) eight months before launch or up to 15 kg (33 lb) on the launch site. (en) FG-46 (AKA EPKM dan SPAB-170) adalah motor roket spin padat stabil Cina berbahan bakar HTPB. Roket ini dikembangkan oleh China Hexi Chemical and Machinery Corporation (juga dikenal sebagai Akademi 6 dari CASIC) untuk digunakan dalam Long March 2E di misi GTO. Roket ini pertama terbang sebagai prototipe PKM pada tanggal 16 Juli 1990 pada misi Badr A. Itu misi komersial pertama yang mengorbit AsiaSat 2 pada tanggal 28 November 1995 dan tepat satu bulan kemudian, pada tanggal 28 Desember misi kedua dan terakhir untuk EchoStar 1. (in)
associated	0001-03-02 (xsd:gMonthDay)
burn time	87.0 (second)
casing	Fiberglass
gold:hypernym	Spin
prov:wasDerivedFrom	wikipedia-en:FG-46?oldid=1084019220&ns=0
page length (characters) of wiki page	4592 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:FG-46
is Link from a Wikipage to another Wikipage of	Long March 2E EchoStar I FG-36 AsiaSat 2 EPKM SpaB-170
is Wikipage redirect of	EPKM SpaB-170
is successor of	FG-36
is launch vehicle of	AsiaSat 2
is foaf:primaryTopic of	wikipedia-en:FG-46

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