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Launch Startup Deep Blue Aerospace Nebula-1 Rocket Second Stage Vacuum Engine “Thunder RV” Integrated Test

On February 22, 2025, Deep Blue Aerospace successfully conducted the second 340-second full-system test of its self-developed "Thunder RV" liquid oxygen kerosene vacuum engine, designed for the second stage of the Nebula-1 rocket, at the liquid rocket engine testing facility in Jinan, Shandong.
During the 340‑second test run, the maximum temperature at the thrust chamber’s outlet reached 1100 K. Over 285 seconds of dynamic vector precision control, 135 oscillations were executed with rapid and stable responses, and the oscillation servo actuation delay did not exceed 0.03 seconds.
This test validated the rationality and reliability of the engine design.

On February 22, 2025, Deep Blue Aerospace successfully conducted the second 340-second full-system test of its self-developed "Thunder RV" liquid oxygen kerosene vacuum engine, designed for the second stage of the Nebula-1 rocket, at the liquid rocket engine testing facility in Jinan, Shandong.
During the 340‑second test run, the maximum temperature at the thrust chamber’s outlet reached 1100 K. Over 285 seconds of dynamic vector precision control, 135 oscillations were executed with rapid and stable responses, and the oscillation servo actuation delay did not exceed 0.03 seconds.
This test validated the rationality and reliability of the engine design.