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EntityQ1564032· pop 13· linked from 212 articles

Also known as HM-7B, HM7-B

The HM7B was a European cryogenic upper stage rocket engine used on the vehicles in the Ariane rocket family. It was replaced by Vinci, which acts as the new upper stage engine on Ariane 6. Nearly 300 engines have been produced to date.

Key facts

Rocket engine.status
Retired
Rocket engine.type
liquid
Rocket engine.oxidiser
LOX
Rocket engine.successor
Vinci
Rocket engine.name
HM7B
Rocket engine.image
SNECMA HM7B rocket engine.jpg
Rocket engine.country_of_origin
France
Rocket engine.first_date
24 December 1979
Rocket engine.designer
Snecma
Rocket engine.manufacturer
Snecma
Rocket engine.purpose
Upper stage engine
Rocket engine.predecessor
HM4
Rocket engine.mixture_ratio
5:1
Rocket engine.cycle
Gas-generator
Rocket engine.combustion_chamber
1
Rocket engine.nozzle_ratio
83.1:1

via Wikipedia infobox

Wikidata facts

Diameter
1.00
Mass
155
Image
CNES 2011 044.jpg
Height
1.80
Show 4 more facts
Commons category
HM-7B
first flight
1984-08-04
maximum thrust
43.6
specific impulse by weight
310
Sources (4)

via Wikidata · CC0

~2 min read

Article

5 sections
Contents
  • History
  • Overview
  • See also
  • Comparable engines
  • References

The HM7B was a European cryogenic upper stage rocket engine used on the vehicles in the Ariane rocket family. It was replaced by Vinci, which acts as the new upper stage engine on Ariane 6. Nearly 300 engines have been produced to date.

==History== The development of HM7 engine begun in 1973 on a base of HM4 rocket engine. It was designed to power a third stage of newly constructed Ariane 1, the first launch system for European Space Agency. Maiden flight took place on 24 December 1979 successfully placing CAT-1 satellite on the orbit. With the later introduction of Ariane 2 and Ariane 3 it became necessary to improve the performance of the upper stage engine. This was achieved by extending the nozzle length and increasing the chamber pressure from 30 to 35 bar, increasing the engine's specific impulse and resulting in a nominal burn time increase from 570 to 735 seconds. Qualification tests were completed in 1983 and this upgraded variant was designated HM7B. It was also used on the Ariane 4 vehicle's upper stage where the burn time was further increased to 780 seconds, and since 12 February 2005 it's also used on the upper stage of Ariane 5 ECA.

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