Chamber/single nozzle
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Notional LOx/LH2 rocket engine. Study 1963. Before moving to favored plug nozzle designs, Bono at Douglas considered having multiple combustion chambers exhaust into a single large nozzle to obtained Improved Specific Impulse.
Used in Nova DAC ISI, ROOS ISI, OOST ISI, and DAC Helios ISI designs. Status: Study 1963. Operational date would have been July 1977. Values shown were maximum considered.
Related
- Country
- USA
- Launch Vehicles
- DAC Helios, DAC Helios ISI, Nova DAC ISI, OOST ISI, ROOST ISI
- Propellants
- Lox/LH2