NASA NTRS · 19870016682
Uprated OMS engine for upper stage propulsion
Abstract
The results of a pre-development component demonstration program on the use of a gas generator-driven turbopump that increases the Space Shuttle's Orbital Maneuvering Engine (OME) operating pressure are given. Tests and analysis confirm the the capability of the concept to meet or exceed performance and life requirements. Storable propellant upper stage concepts are also discussed.
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Boyd, William C.. 1986-08-01. Uprated OMS engine for upper stage propulsion. https://ntrs.nasa.gov/citations/19870016682
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