BT-4 (rocket engine)

http://dbpedia.org/resource/BT-4_(rocket_engine)

The BT-4 is a pressure-fed liquid rocket engine designed and manufactured by IHI Aerospace of Japan. It was originally developed for the LUNAR-A project, but it has been used as a liquid apogee engine in some geostationary communications satellite based on the Lockheed Martin A2100 and GEOStar-2 satellite buses. It has also been used on the HTV and Cygnus automated cargo spacecraft. rdf:langString
BT-4はIHIエアロスペース(旧石川島播磨重工業航空宇宙事業部)が開発し、製造している推力500N級の2液式ロケットエンジンである。 rdf:langString
rdf:langString BT-4 (rocket engine)
rdf:langString BT-4
rdf:langString BT-4
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rdf:langString Japan
rdf:langString In production
rdf:langString liquid
rdf:langString The BT-4 is a pressure-fed liquid rocket engine designed and manufactured by IHI Aerospace of Japan. It was originally developed for the LUNAR-A project, but it has been used as a liquid apogee engine in some geostationary communications satellite based on the Lockheed Martin A2100 and GEOStar-2 satellite buses. It has also been used on the HTV and Cygnus automated cargo spacecraft.
rdf:langString BT-4はIHIエアロスペース(旧石川島播磨重工業航空宇宙事業部)が開発し、製造している推力500N級の2液式ロケットエンジンである。
xsd:nonNegativeInteger 15332

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