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Daniel-2
N2O4/UDMH propellant rocket stage.

Status: Retired 1961. Gross mass: 2,000 kg (4,400 lb). Height: 4.50 m (14.70 ft). Diameter: 0.80 m (2.62 ft).

Subtopics
Jericho-1-1 N2O4/UDMH propellant rocket stage.
Country: France. Engines: MD-620 engine. Launch Vehicles: Daniel, MD-620. Propellants: N2O4/UDMH. Agency: Dassault.
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