| 词条 | FG-36 |
| 释义 |
|name =FG-15B |image = |image_size = |caption = |country_of_origin=China |date = |first_date =1986-02-02 |last_date = |designer =China Hexi Chemical and Machinery Corporation |manufacturer = |purpose =Apogee kick motor |associated =Long March 1D |predecessor =FG-15 |successor =FG-46 |status =Out of Production |type =solid |oxidiser = |fuel =HTPB |grain = |core = |casing = |nozzle = |description = |combustion_chamber=1 |nozzle_ratio = |thrust = |thrust_at_altitude= |thrust(Vac) ={{convert|44|kN|lbf|abbr=on}} |thrust(SL) = |thrust_to_weight= |chamber_pressure= |specific_impulse= |specific_impulse_vacuum={{convert|289|isp|abbr=on}} |specific_impulse_sea_level= |total_impulse ={{convert|1.842|MN|abbr=on}} |burn_time =43s |gimbal = |capacity ={{convert|650|kg|lb|abbr=on}} |dimensions = |length ={{convert|1529|mm|in|abbr=on}} |diameter ={{convert|896|mm|in|abbr=on}} |dry_weight ={{convert|79|kg|lb|abbr=on}} |used_in =Fengyun 2 APK and Long March 1D third stage. |references =[2][3][4] |notes = }} The FG-36 (AKA Fengyun 2 AKM) was a Chinese spin stabilized apogee kick motor burning HTPB. It was developed by China Hexi Chemical and Machinery Corporation (also known as the 6th Academy of CASIC) for use in the Fengyun 2 satellite bus for insertion into GSO orbit.[3][8] It has a total nominal mass of {{convert|729|kg|lb|abbr=on}}, of which {{convert|650|kg|lb|abbr=on}} is propellant load and its burn out mass is {{convert|79|kg|lb|abbr=on}}. It has an average thrust of {{convert|44|kN|lbf|abbr=on}} with a specific impulse of 289 seconds burning for 43 seconds, with a total impulse of {{convert|1.842|MN|abbr=on}}. While it was designed as an apogee kick motor and as such it flew in spin stabilized mode, it was also adapted to the Long March 1D third stage. It was paired with a RCS in a similar solution to the CTS.[2][4] See also
References1. ^1 2 {{cite web |url=http://www.b14643.de/Spacerockets_1/China/CZ-1/Description/Text.htm |title=Chang Zheng CZ-1 & CZ-1D |website=B14643.DE |author=Norbert Bgügge |accessdate=2015-07-25}} [1][2][3][4]2. ^1 2 {{cite web |url=http://space.skyrocket.de/doc_sdat/fy-2.htm |title=CZ-1 (Chang Zheng-1) |publisher=Gunter's Space Page |author=Gunter Dirk Krebs |accessdate=2015-07-25}} 3. ^1 {{cite book |url=https://books.google.com.ar/books?id=hZBAAAAAQBAJ&pg=PA97&lpg=PA97&dq=GF-36 |title=China's Space Program — The Great Leap Forward |last=Harvey |first=Brian |chapter=Rocket Engines |page=97 |publisher=Springer Science & Business Media |date=2013 |isbn=978-1461450436 |access-date=2015-07-25}} 4. ^1 2 {{cite web |url=http://sinodefence.com/rocketry/cz1/ |title=Chang Zheng-1 |publisher=SinoDefence |accessdate=2015-07-25 |deadurl=yes |archiveurl=https://web.archive.org/web/20150716083542/http://sinodefence.com/rocketry/cz1/ |archivedate=2015-07-16 |df= }} }}{{Orbital spacecraft rocket engines}}{{Rocket engines}}{{DEFAULTSORT:FG-36}}{{rocket-stub}} 2 : Rocket engines of China|Solid-fuel rockets |
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