Matches in DBpedia 2016-04 for { <http://wikidata.dbpedia.org/resource/Q22127563> ?p ?o }
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- Q22127563 subject Q7008567.
- Q22127563 subject Q8672072.
- Q22127563 subject Q8759915.
- Q22127563 abstract "The FG-15 (AKA DFH-2 AKM and SpaB-170) 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 Dong Fang Hong 2 satellite bus for insertion into GSO orbit.It has a total nominal mass of 580 kg (1,280 lb), of which 505 kg (1,113 lb) is propellant load and its burn out mass is 75 kg (165 lb). It has an average thrust of 40.9 kN (9,200 lbf) with a specific impulse of 289 seconds burning for 35 seconds, with a total impulse of 1.432 MN (322,000 lbf). This motor introduced a series of innovations for the Chinese solid motor industry: first use of glass fibre wound cases, carbon/carbon nozzle throat insert material, contoured divergent nozzle, and non-destructive test of the motor grain.The initial version had the manufacturing code FG-15 was associated to the DFH-2 bus and flew twice. The FG-15B was used by the DFH-2A bus and flew five times.".
- Q22127563 wikiPageWikiLink Q10874081.
- Q22127563 wikiPageWikiLink Q148.
- Q22127563 wikiPageWikiLink Q1778579.
- Q22127563 wikiPageWikiLink Q192316.
- Q22127563 wikiPageWikiLink Q21714922.
- Q22127563 wikiPageWikiLink Q3115617.
- Q22127563 wikiPageWikiLink Q51504.
- Q22127563 wikiPageWikiLink Q53734.
- Q22127563 wikiPageWikiLink Q618844.
- Q22127563 wikiPageWikiLink Q7008567.
- Q22127563 wikiPageWikiLink Q7224880.
- Q22127563 wikiPageWikiLink Q734306.
- Q22127563 wikiPageWikiLink Q7577350.
- Q22127563 wikiPageWikiLink Q837858.
- Q22127563 wikiPageWikiLink Q8672072.
- Q22127563 wikiPageWikiLink Q8759915.
- Q22127563 wikiPageWikiLink Q936190.
- Q22127563 comment "The FG-15 (AKA DFH-2 AKM and SpaB-170) 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 Dong Fang Hong 2 satellite bus for insertion into GSO orbit.It has a total nominal mass of 580 kg (1,280 lb), of which 505 kg (1,113 lb) is propellant load and its burn out mass is 75 kg (165 lb).".
- Q22127563 label "FG-15".