FG-47
Appearance
Country of origin | China |
---|---|
First flight | 1997-09-01 |
Designer | China Hexi Chemical and Machinery Corporation |
Application | Kick engine |
Associated LV | Long March 2C CTS |
Status | In Production |
Solid-fuel motor | |
Propellant | HTPB |
Performance | |
Thrust, vacuum | 9.8 kN (2,200 lbf) |
Specific impulse, vacuum | 288 s (2.82 km/s) |
Total impulse | 353 kN (79,000 lbf) |
Burn time | 36s |
Dimensions | |
Length | 852 mm (33.5 in) |
Diameter | 542 mm (21.3 in) |
Used in | |
CTS | |
References | |
References | [1][2][3] |
The FG-47 (a.k.a. SpaB-54) is a Chinese solid rocket motor burning HTPB.[1][4] 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.[1][2][5][6]
It has a total nominal mass of 160 kg (350 lb), of which 125 kg (276 lb) is propellant load. It has an average thrust of 9.8 kN (2,200 lbf) with a specific impulse of 288 seconds burning for 35 seconds, with a total impulse of 353 kN (79,000 lbf).
See also
References
- ^ a b c Norbert Bgügge. "Some Chinese solid fuel aerospace motors". B14643.DE. Archived from the original on 2015-09-26. Retrieved 2015-07-25.
- ^ a b "Chapter 2.4 — CTS Introduction". LM-2C User's Manual. Issue 1999. CASC. 1999. pp. 2–15. Retrieved 2015-07-08.
- ^ "CZ-2C/SD". Encyclopedia Astronautica. Archived from the original on 2016-03-04. Retrieved 2015-07-25.
- ^ "SpaB-54". Encyclopedia Astronautica. Archived from the original on 2015-08-24. Retrieved 2015-07-25.
- ^ Norbert Bgügge. "Propulsion CZ-2E, CZ-2F". B14643.DE. Retrieved 2015-07-25.
- ^ Krebs, Gunter Dirk (2013-09-21). "CZ-2C (2) SD (Chang Zheng-2C (2) SD)". Retrieved 2015-07-25.