Atlas LV-3 Agena A

The American orbital launch vehicle. Atlas D + 1 x Agena A upper stage. Agena originally called 'Hustler', based on engine for cancelled rocket-propelled nuclear warhead pod for B-58 Hustler bomber.
AKA: Atlas-Hustler;LV-3A. Status: Retired 1961. First Launch: 1960-02-26. Last Launch: 1961-01-31. Number: 4 . Payload: 800 kg (1,760 lb). Thrust: 1,587.19 kN (356,815 lbf). Gross mass: 123,990 kg (273,350 lb). Height: 30.00 m (98.00 ft). Diameter: 3.05 m (10.00 ft). Apogee: 600 km (370 mi).

Payload: 800 kg (1,760 lb) to a GTO.

Stage Data - Atlas LV-3A / Agena A

Stage 0. 1 x Atlas MA-2. Gross Mass: 3,050 kg (6,720 lb). Empty Mass: 3,050 kg (6,720 lb). Thrust (vac): 1,517.422 kN (341,130 lbf). Isp: 282 sec. Burn time: 135 sec. Isp(sl): 248 sec. Diameter: 4.90 m (16.00 ft). Span: 4.90 m (16.00 ft).Propellants: Lox/Kerosene. No Engines: 2. Engine: XLR-89-5. Status: Out of Production.
Stage 1. 1 x Atlas Agena LV-3A. Gross Mass: 117,150 kg (258,270 lb). Empty Mass: 2,390 kg (5,260 lb). Thrust (vac): 363.218 kN (81,655 lbf). Isp: 309 sec. Burn time: 330 sec. Isp(sl): 215 sec. Diameter: 3.05 m (10.00 ft). Span: 4.90 m (16.00 ft). Length: 20.27 m (66.50 ft). Propellants: Lox/Kerosene. No Engines: 1. Engine: XLR-105-5. Status: Out of Production.
Stage 2. 1 x Agena A. Gross Mass: 3,790 kg (8,350 lb). Empty Mass: 885 kg (1,951 lb). Thrust (vac): 68.950 kN (15,501 lbf). Isp: 276 sec. Burn time: 120 sec. Diameter: 1.52 m (4.98 ft). Span: 1.52 m (4.98 ft). Length: 4.73 m (15.51 ft). Propellants: Nitric acid/UDMH. No Engines: 1. Engine: Bell 8048. Other designations: RM-81. Status: Out of Production.