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Hybrid
| R-13 engine Dushkin Nitric acid/Solid hybrid rocket engine. Out of Production. Developed in the late 1950s by OKB Dushkin. It was a combined (powder+liquid) engine, characterized by a new technical approach conceived by Dushkin in the prewar design of the KRD-604. |
 | Dolphin American sea-launched test vehicle. The Dolphin hybrid rocket (solid fuel and liquid oxygen oxidizer) was built by Starstruck (formerly ARC Technology), a predecessor to AMROC. The Dolphin included not only innovative propulsion technology but was also launched from a floating launch canister at sea. One test article of the hybrid was successfully launched in the summer of 1984. But the project was backed entirely with private funds and when backing for further development was not forthcoming, the project folded. |
| Falcon SLV-1 Michoud LOx/Solid hybrid rocket engine. First stage. Study 2005. Part of the USAF FALCON program to assess hybrid propulsion applications for a responsive small launch vehicle. |
| Falcon SLV-2 Michoud hybrid rocket LOx/Solid engine. Upper stages. Study 2005. Part of the USAF FALCON program to assess hybrid propulsion applications for a responsive small launch vehicle. |
| Hyperion engine eAc hybrid N2O/Solid rocket engine. |
| H1500 Notional LOx/Solid hybrid rocket engine. Design 1988. Used on Industrial Launch Vehicle launch vehicle. |
| HTR Nammo LOx/Solid hybrid rocket engine. |
| KRD-604 Dushkin Nitric acid/Solid hybrid rocket engine. Out of Production. The KRD-604 engine was developed in the late 1930s by OKB Dushkin. It was a combined (powder+liquid) engine, characterized by a new technical approach. |
| MTV Motor SpaceDev N2O/Solid hybrid rocket engine. Upper stages. Small hybrid rocket motor designed for use in the Maneuver and Transfer Vehicle, an upper stage orbital transfer motor. Tested 2001. |
| SBIR Hybrid SpaceDev N2O/Solid hybrid rocket engine. First stage. Upper-stage hybrid propulsion system, part of 2004 Phase 2 of SBIR contract from AFRL for a hybrid rocket motor-based small launch vehicle project. |
| SpaceDev Hybrid SpaceDev N2O/Solid hybrid rocket engine. Rocketplane boost. Out of production. Used on Tier One launch vehicle. First flight 2002. |
| HYSR-1 LOx/Solid propellant rocket stage. Thrust 270.00 kN. |
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