HG-3
Rocket engine
The HG-3 was a liquid-fuel cryogenic rocket engine which was designed for use on the upper stages of Saturn rockets in the post-Apollo era. Wikipedia
Specific impulse, sea-level: 280 seconds (2.7 km/s)
Thrust, sea-level: 869.6 kN (195,500 lbf)
The HG-3 was a liquid-fuel cryogenic rocket engine which was designed for use on the upper stages of Saturn rockets in the post-Apollo era.
Part of: LL-100 blood cancer cell line panel. Characteristics: Genetically heterogeneous, consists of 3 subclones (PubMed=27566572). Doubling time: ~50-70 hours ...
The HG-3 was an American upper stage hydrogen/oxygen engine family. The HG-3 engines were built by Rocketdyne at their Canoga plant.
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