
Jiangsu, China
2016
Space Transportation, Launch Services, Rocket Manufacturing, Aerospace Engineering, Propulsion Systems, Satellite Launch Services
Deep Blue Aerospace is a commercial space technology company developing reusable orbital launch vehicles and liquid-fueled rocket engines. Its engineering programs focus on vertical takeoff and vertical landing, liquid oxygen and kerosene propulsion, and the recovery and reuse of rocket first stages.
Founded in 2016, the company develops the Nebula series of launch vehicles and Thunder series of rocket engines. Its technologies are intended to support commercial satellite deployment through launch systems that can be recovered, refurbished, and flown on subsequent missions.
Deep Blue Aerospace designs, manufactures, and tests liquid-propellant rockets for delivering satellites and other payloads into Earth orbit. Its engineering work covers rocket structures, propulsion systems, flight control, stage separation, engine integration, and reusable booster recovery.
The company’s Nebula-1 rocket is designed to carry approximately two metric tons to low Earth orbit in its initial configuration. Its first stage uses multiple Thunder-R engines and is designed to return through a controlled vertical landing after launch.
Deep Blue Aerospace is also developing the larger Nebula-2 launch vehicle, which is intended to provide substantially greater payload capacity using more powerful Thunder-RS engines.
Its propulsion development includes engine combustion testing, turbopump systems, thrust regulation, restart capability, and additive manufacturing of rocket components. The company conducts ground firing and flight testing to evaluate the performance of its reusable launch technologies.
Deep Blue Aerospace has also outlined commercial launch services, including dedicated satellite launches and shared missions. These offerings remain dependent on successful orbital qualification and operational deployment of its launch vehicles.
Deep Blue Aerospace develops liquid oxygen and kerosene rocket propulsion systems and reusable launch vehicle architectures. Its engineering work focuses on high-thrust liquid rocket engines, controlled descent, vertical landing, and the recovery of rocket stages for subsequent flights.
Nebula-1 is designed as a two-stage orbital rocket with nine Thunder-R engines powering its first stage. Its reusable configuration incorporates engine throttling, restart capability, flight control, and landing maneuvers. During descent, the first stage must reduce velocity and control its position before touching down vertically.
The company’s Thunder-R engine uses an open-cycle gas-generator architecture with liquid oxygen and kerosene propellants. Its published specifications include approximately 237 kilonewtons of sea-level thrust and 268 kilonewtons of vacuum thrust, although some company pages show different values for later configurations. The engine incorporates thrust regulation, restart capability, and additively manufactured components.
The larger Thunder-RS engine is designed for Nebula-2. Its published specifications include approximately 1,300 kilonewtons of sea-level thrust and 1,500 kilonewtons in vacuum. A reported August 2026 hot-fire test produced approximately 1,297.5 kilonewtons over a 100-second test period.
Deep Blue Aerospace also uses metal additive manufacturing and integrated turbopump engineering to produce complex engine components and reduce manufacturing complexity. Its engine designs incorporate gas-generator combustion, propellant feed systems, thrust-vector control, and regulated combustion conditions.
The September 2024 Nebula-1 high-altitude test demonstrated powered ascent and controlled descent, but the landing sequence failed near touchdown. The company subsequently conducted additional engine and integrated propulsion testing, including a nine-engine first-stage ground firing in November 2025.
Reusable rockets have changed the economics of commercial space transportation by allowing expensive launch vehicle hardware to be recovered instead of discarded after a single mission.
Deep Blue Aerospace is developing domestically manufactured reusable launch systems that could expand commercial access to orbit if its rockets achieve successful flight qualification and repeatable recovery.
Its propulsion development, including the Thunder-R and Thunder-RS engines, contributes to the engineering capabilities required for higher-capacity launch vehicles and reusable rocket operations.
The company’s test programs also illustrate the technical challenges of vertical booster recovery, where engine restart, thrust regulation, guidance, and landing control must operate together under demanding flight conditions.
Deep Blue Aerospace is relevant to the growing commercial launch market because its development programs target satellite deployment and launch vehicle reusability. However, its planned commercial capabilities should be distinguished from demonstrated orbital launch and recovery performance.
Nebula-1 is a two-stage liquid oxygen and kerosene launch vehicle designed to deliver approximately two metric tons of payload to low Earth orbit in its initial configuration. Its first stage incorporates nine Thunder-R engines and is designed for vertical landing and reuse. Development activities have included high-altitude flight testing, engine qualification, and integrated first-stage ground firing. A successful orbital mission has not yet been independently confirmed.
Nebula-2 is a larger reusable orbital launch vehicle under development. Its design incorporates higher-thrust Thunder-RS engines and a recoverable first-stage architecture. Published development information identifies a planned payload capacity of approximately 25 metric tons to low Earth orbit, although the final vehicle configuration and demonstrated performance remain subject to flight testing.
Thunder-R is a liquid oxygen and kerosene rocket engine developed for the Nebula-1 launch vehicle. It uses an open-cycle gas-generator configuration and incorporates thrust regulation, restart capability, and additively manufactured components. Published specifications for one configuration include approximately 237 kilonewtons of sea-level thrust and 268 kilonewtons in vacuum. The engine family has undergone individual and clustered ground testing.
Thunder-RS is a higher-thrust liquid rocket engine developed for the Nebula-2 program. It uses liquid oxygen and kerosene propellants and incorporates gas-generator combustion, turbopump systems, and thrust regulation. Published specifications identify approximately 1,300 kilonewtons of sea-level thrust and 1,500 kilonewtons in vacuum. A long-duration hot-fire test was reported in August 2026.
Deep Blue Aerospace is developing vertical takeoff and vertical landing technology for reusable rocket boosters. The recovery architecture combines controlled engine throttling, flight guidance, attitude stabilization, descent management, and landing control. A September 2024 high-altitude test demonstrated several stages of the flight sequence but ended in a hard landing, leaving reliable recovery and reuse unproven.
Deep Blue Aerospace has outlined commercial launch offerings for dedicated satellite deployment and shared payload missions. Its proposed services include mission-specific orbital planning, launch vehicle integration, and satellite transportation to low Earth orbit. Operational availability depends on successful launch vehicle qualification and the establishment of repeatable orbital launch capability.
Commercial Satellite Launch: Developing rockets intended to transport commercial and institutional satellites into Earth orbit.
Reusable Space Transportation: Testing rocket recovery and refurbishment technologies intended to reduce the hardware consumed during successive launches.
Satellite Constellation Deployment: Developing launch capacity for groups of satellites used in communications, Earth observation, and other orbital services.
Rocket Engine Manufacturing: Producing liquid-propellant engines incorporating turbopumps, gas generators, thrust regulation, and additive manufacturing.
Vertical Landing Research: Evaluating propulsion, guidance, and control systems required for reusable booster recovery.
Dedicated Launch Missions: Planning launch services configured around specific payload and orbital requirements.
Shared Satellite Launches: Developing missions that accommodate payloads from multiple customers aboard a single rocket.
Deep Blue Aerospace develops reusable orbital launch vehicles, liquid-fueled rocket engines, and supporting propulsion technologies for commercial satellite launch missions.
Deep Blue Aerospace was founded in 2016. Its principal development activities include reusable rocket engineering, liquid propulsion, and commercial launch systems.
Nebula-1 is a two-stage rocket designed to deliver approximately two metric tons to low Earth orbit. Its first stage uses nine Thunder-R engines and incorporates a planned vertical recovery system.
A September 2024 high-altitude test demonstrated powered ascent and controlled descent, but the vehicle suffered a hard landing near touchdown. A successful recovery and reuse of an orbital booster has not been independently confirmed.
The company develops the Thunder-R and Thunder-RS liquid oxygen and kerosene rocket engines. Thunder-R supports the Nebula-1 program, while the higher-thrust Thunder-RS is being developed for Nebula-2.
Nebula-1 is a smaller reusable rocket designed for approximately two metric tons of payload to low Earth orbit. Nebula-2 is a larger launch vehicle under development, with a planned payload capacity of approximately 25 metric tons.
Deep Blue Aerospace has conducted rocket flight and propulsion tests, including a high-altitude recovery test in 2024 and subsequent engine testing. As of November 2026, a successful orbital launch has not been independently confirmed.
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