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Delta P
Part of Delta Family
N2O4/Aerozine-50 propellant rocket stage. .

AKA: TR-201. Status: Retired 1988. Thrust: 41.92 kN (9,425 lbf). Gross mass: 5,434 kg (11,979 lb). Unfuelled mass: 820 kg (1,800 lb). Specific impulse: 301 s. Burn time: 322 s. Height: 5.97 m (19.58 ft). Diameter: 1.38 m (4.52 ft). Span: 1.38 m (4.52 ft).

Cost $ : 4.350 million.



Country: USA. Engines: TR-201. Launch Vehicles: Delta 1914, Delta 2313, Delta 2914, Delta 2310, Delta 2910, Delta 1410, Delta 2913, Delta 3914, Delta 3910, Delta 3910/PAM, Delta 3913. Propellants: N2O4/Aerozine-50.

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