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R-4D

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EntityQ11240350· pop 8· linked from 158 articles

Also known as Marquardt R-4D, Aerojet R-4D

The R-4D is a small hypergolic rocket engine, originally designed by Marquardt Corporation for use as a reaction control system thruster on vehicles of the Apollo crewed Moon landing program. Aerojet Rocketdyne manufactures and markets modern versions of the R-4D.

Wikidata facts

Country of origin
United States
Manufacturer
Aerojet Rocketdyne
Image
Apollo RCS quad.jpg
Show 4 more facts
inception
1960-00-00
source of energy
hypergolic propellant
Commons category
R-4D (rocket engine)
Sources (4)

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Encyclopedic overview

4 sections
Contents
  • History
  • Design
  • Additional literature
  • References

The R-4D is a small hypergolic rocket engine, originally designed by Marquardt Corporation for use as a reaction control system thruster on vehicles of the Apollo crewed Moon landing program. Aerojet Rocketdyne manufactures and markets modern versions of the R-4D.

==History== Developed as an attitude control thruster for the Apollo Command/Service Module and Lunar Module in the 1960s, each unit for the modules employed four quadruple clusters (pods). It was first flown on AS-201 in February 1966. Approximately 800 were produced during the Apollo program.

Excerpted from Wikipedia’s “R-4D” article, available under the CC BY-SA 4.0 licence.

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