Daytona-E

Phantom Space Corporation

The Phantom Daytona is a two-stage pump-fed launcher capable of placing 450 kg into a low inclination orbit and 370 kg into a polar orbit. The oxidizer-rich stage combustion LOX/RP engines have completed flight qualification, are ready for integration and include a full complement of thrust vector control and engine controllers for each engine.
The Phantom Daytona launch vehicle uses seven qualified 5,000 lbf  "Hadley"engines from Ursa Major Technologies on the first stage, a single "Hadley" vacuum engine on the second stage as common vendor/lowest cost approach.

The "Hadley" engine is a 5,000 lbf thrust, pump fed, lox-kerosene oxygen-rich staged combustion engine. "Hadley" features active throttle and thrust vector control entirely managed by its internal engine controllers. The engine controller receives power from the vehicle and relays it to valves and actuators. It receives thrust and thrust vectoring commands from the vehicle and commands engine valves and actuators accordingly to target the commanded value.