LE-7

The LE-7 and its succeeding upgrade model the LE-7A were staged combustion cycle LH₂/LOX liquid rocket engines produced in Japan for the H-II series of launch vehicles. Design and production work was all done domestically in Japan, the first major (main/first-stage) liquid rocket engine with that claim, in a collaborative effort from the National Space Development Agency (NASDA), Aerospace Engineering Laboratory (NAL), Mitsubishi Heavy Industries, and Ishikawajima-Harima. NASDA and NAL have since been integrated into JAXA. However, a large part of the work was contracted to Mitsubishi, with Ishikawajima-Harima providing turbomachinery, and the engine is often referred to as the Mitsubishi LE-7(A).

MainWikipediaGalleryBibliographyTableSearch

Wikimedia, Wikidata
cryogenic rocket engine, 
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Sweden, Tarshish, cryogenic rocket engine, Dong Fang Hong 2, Ekran, A, 

​ ​

Location: KML, Cluster Map, Maps,

• 

  LE-7A ⓘ
  Japanese cryogenic liquid-fuel rocket engine

Frameless

LE-7 rocket engine

LE-7-join-to-H-II-GTV

H-IIRocket F8 LE-7engine

Mitsubishi Minatomirai Industrial Museum @ Yokohama (9054512140)

1st floor of Nagoya City Science Museum 20150125

LE-7 engine on 1st floor of Nagoya City Science Museum

NASDA - NAL - Mitsubishi - Ishikawajima-Harima LE-7 Rocket engine 20200313

Type	Subtype	Date	Description	Notes	Source
class	rocket engine	2001	LE-7A	LE-7	Wikidata
commons	image		LE-7 rocket engine		Commons
commons	image		LE-7-join-to-H-II-GTV		Commons
commons	image		H-IIRocket F8 LE-7engine		Commons
commons	image		Mitsubishi Minatomirai Industrial Museum @ Yokohama (9054512140)		Commons
commons	image		1st floor of Nagoya City Science Museum 20150125		Commons
commons	image		LE-7 engine on 1st floor of Nagoya City Science Museum		Commons
commons	image		NASDA - NAL - Mitsubishi - Ishikawajima-Harima LE-7 Rocket engine 20200313		Commons