FG-47

{{Infobox rocket engine

|name =FG-47

|image =

|image_size =

|caption =

|country_of_origin=China

|date =

|first_date =1997-09-01

|last_date =

|designer =China Hexi Chemical and Machinery Corporation

|manufacturer =

|purpose =Kick engine

|associated =Long March 2C CTS

|predecessor =

|successor =

|status =In Production

|type =solid

|oxidiser =AP

|fuel =HTPB

|grain =

|core =

|casing =

|nozzle =

|description =

|combustion_chamber=

|nozzle_ratio =

|thrust =

|thrust_at_altitude=

|thrust(Vac) ={{convert|9.8|kN|lbf|abbr=on}}

|thrust(SL) =

|thrust_to_weight=

|chamber_pressure=

|specific_impulse=

|specific_impulse_vacuum={{convert|288|isp|abbr=on}}

|specific_impulse_sea_level=

|total_impulse ={{convert|353|kN|abbr=on}}

|burn_time =36s

|gimbal =

|capacity =

|dimensions =

|length ={{convert|852|mm|in|abbr=on}}

|diameter ={{convert|542|mm|in|abbr=on}}

|dry_weight =

|used_in =CTS

|references =

|notes =

}}

The FG-47 (a.k.a. SpaB-54) is a Chinese solid rocket motor burning HTPB-based composite propellant. It was developed by China Hexi Chemical and Machinery Corporation (also known as the 6th Academy of CASIC) for use in the Long March 2C SD/CTS/SMA third stage. It had its inaugural flight on the Iridium-MFS demonstration mission on September 1, 1997.

It has a total nominal mass of {{convert|160|kg|lb|abbr=on}}, of which {{convert|125|kg|lb|abbr=on}} is propellant load. It has an average thrust of {{convert|9.8|kN|lbf|abbr=on}} with a specific impulse of 288 seconds burning for 35 seconds, with a total impulse of {{convert|353|kN|abbr=on}}.

See also

References

{{reflist|30em|refs=

{{cite web |url=http://www.b14643.de/Spacerockets_1/China/CZ-2EF/Propulsion/engines.htm |title=Propulsion CZ-2E, CZ-2F |website=B14643.DE |author=Norbert Bgügge |access-date=2015-07-25}}

{{cite web |url=http://www.b14643.de/Spacerockets/Diverse/SpaB_aerospace_motors/index.htm |title=Some Chinese solid fuel aerospace motors |website=B14643.DE |author=Norbert Bgügge |access-date=2015-07-25 |url-status=dead |archive-url=https://web.archive.org/web/20150926034320/http://www.b14643.de/Spacerockets/Diverse/SpaB_aerospace_motors/index.htm |archive-date=2015-09-26 }}

{{cite book |url=http://fas.org/spp/guide/china/launch/lm2c/2C_Chapter2.htm |title=LM-2C User's Manual. Issue 1999 |date=1999 |publisher=CASC |chapter=Chapter 2.4 — CTS Introduction |pages=2–15 |access-date=2015-07-08}}

{{cite web |url=http://www.astronautix.com/lvs/cz2csd.htm |title=CZ-2C/SD |publisher=Encyclopedia Astronautica |access-date=2015-07-25 |url-status=dead |archive-url=https://web.archive.org/web/20160304001906/http://www.astronautix.com/lvs/cz2csd.htm |archive-date=2016-03-04 }}

{{cite web |url=http://www.astronautix.com/engines/spab54.htm |title=SpaB-54 |publisher=Encyclopedia Astronautica |access-date=2015-07-25 |url-status=dead |archive-url=https://web.archive.org/web/20150824113736/http://www.astronautix.com/engines/spab54.htm |archive-date=2015-08-24 }}

{{cite web |url=http://space.skyrocket.de/doc_lau_det/cz-2c-2-sd.htm |title=CZ-2C (2) SD (Chang Zheng-2C (2) SD) |last=Krebs |first=Gunter Dirk |date=2013-09-21 |access-date=2015-07-25}}

}}

{{Rocket engines}}

{{DEFAULTSORT:FG-47}}

Category:Rocket engines of China

Category:Solid-fuel rockets

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