
深蓝航天 Deep Blue Limited – Deep Blue Aerospace Landspace One of sixty Chinese private space Carrier Rocket Companies in China-People’s Republic of China… As many of sixty plus Private Rocket Deep Blue Aerospace Co., Ltd. was established in 2017. The company is mainly a high-tech aerospace enterprise that focuses on the direction of liquid recovery and reusable launch vehicles and provides users with commercial launch services. Deep Blue Aerospace Co., Ltd. is headquartered in Nantong City, Jiangsu Province. At the same time, the company has rocket general and liquid engine R&D centers in Yizhuang, Beijing and Xi’an, Shaanxi, respectively, and a rocket power system test base in Tongchuan, Shaanxi…..
Deep Blue Aerospace on the month of forth week September 2026 Nebula-1 Y2 Development Progress | Thunder R2.0 Thrust Jumps to 30-Ton Class, First 200-Second Long-Duration Test Successfully Completed
Recently, DeepBlue Aerospace’s independently developed needle-plug reusable liquid oxygen-kerosene engine, “Thunder R2.0,” completed its power upgrade, increasing its thrust to the 30-ton class, and successfully completed its first 200-second long-duration test. The successful test of the Thunder R2.0 engine will accelerate the improvement of DeepBlue Aerospace’s complete reusable rocket and engine product portfolio, covering multiple scenarios and mission requirements. Based on this, DeepBlue Aerospace will continue to conduct reliability growth tests on the “Thunder” series engines, laying a solid foundation for achieving low-cost, high-frequency space transportation services.
The Thunder R2.0 engine, which powers the DeepBlue Space Nebula-1 Y2 rocket, has just completed a power upgrade, boosting its thrust to 30 tons and successfully completing its first 200-second long-duration test, allowing this rocket, which has not yet made its maiden flight, to directly enter a new stage.

I. Thunder R2.0 Core Upgrade Implemented, Achieving Breakthroughs in Both Thrust and Performance
- Thrust Significantly Increased : The Thunder R2.0 engine’s measured maximum thrust is close to 30 tons, a 50% increase compared to the first-generation model.
- Key parameter optimization : Engine chamber pressure increased from approximately 8 MPa to 10 MPa, and specific impulse performance improved by 10 seconds.
- The structure has been greatly simplified : the number of valves has been reduced by about 1/3, the overall weight has been reduced by about 25%, and the engine thrust-to-weight ratio has been increased from less than 80 to more than 150; the inner wall of the thrust chamber has been upgraded from steel to copper, and the after-processing process has been simplified.2
II. 200-second long-duration test, surpassing the threshold of actual launch load.
- Test nature : This test was the first 200-second long-duration test, which is equivalent to the engine burning continuously for 3 minutes and 20 seconds, fully simulating the intensity of a real launch, rather than a short-term ignition verification.
- Significance of the test : The successful test will accelerate the improvement of DeepBlue Aerospace’s capabilities to meet the needs of multiple scenarios and missions
The Nebula-1 is a medium-sized liquid-fueled reusable launch vehicle independently developed by DeepBlue Aerospace. Currently, the development of its second remote sensing version is underway. Recent key developments are as follows:
Engine Upgrade: Thunder R2.0 Completes First 200-Second Long-Distance Test
DeepBlue Aerospace’s independently developed needle-type reusable liquid oxygen-kerosene engine, “Thunder R2.0,” has completed a power upgrade, with its thrust jumping from the initial 20-ton level of the Thunder R1 to the 30-ton level, and successfully completed its first 200-second long-duration test. Key achievements of this test include: a measured maximum thrust of nearly 30 tons, a 50% increase compared to the first generation; an increase in engine chamber pressure from approximately 8 MPa to 10 MPa, improving specific impulse performance by 10 seconds; a significantly simplified engine structure, reducing the number of valves by about one-third, reducing overall engine weight by about 25%, and increasing the thrust-to-weight ratio from less than 80 to over 150; and an upgrade to a copper inner wall for the thrust chamber, with simultaneous process optimization.

Rocket overall parameters and positioning
The Nebula-1 rocket is approximately 30.2 meters long, has a ground thrust of about 180 tons, and a low Earth orbit payload capacity of about 2 tons. It is positioned as a mainstay commercial launch vehicle for high-frequency missions, targeting small and medium-sized satellite operators, research institutions, and other customers, meeting the needs of rapid networking of small and medium-sized satellites and constellations. The long-term design goal is to increase the thrust of a single engine to the 35-40 ton range and to enable the rocket to be reused 50 times.
Historical Background and Future Prospects
Previously, during its first high-altitude vertical recovery flight test, the Nebula-1 rocket experienced an anomaly during the final landing phase, resulting in a less than successful test. DeepBlue Space has continued its development since then, and in April of this year, Nebula-1 entered the launch site to complete integrated launch and propellant loading system training. The fact that the second version is directly equipped with an upgraded engine indicates that DeepBlue Space is accelerating its technological iteration and striving to achieve its maiden flight as soon as possible.
III. With “Yao-2” taking the lead, the overall development of Nebula-1 has entered the final sprint stage.
- Iteration strategy : In version 1
- Rocket parameters : The Nebula-1 is about 30.2 meters long. It adopts a two-stage configuration and uses a combination of liquid oxygen and kerosene propellants. The first stage is equipped with nine Thunder R-series engines in parallel. Its low Earth orbit payload capacity is about 2 tons.
- Development progress : The first and second stage core power units of the rocket have passed key tests and assessments, and have entered the full sprint stage of the first flight mission. Previously, the parallel test of the nine engines of the first stage power system was completed and the multi-engine collaborative working capability was verified.
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