Vehicle Search

International Launch Services

Russian Federation

Launch Price

No data available

• Performance Summary

  	Angara A3	Angara A5	Angara A5/UOHM
  200 km (108 nmi), 63 deg	14,000 kg (31,000 lbm)	24,500 kg (54,000 lbm)	28,500 kg (62,800 lbm)
  200 km (108 nmi), 90 deg	12,600 kg (27,800 lbm)	22,400 kg (49,000 lbm)	?
  Space Station Orbit: 407 km (220 nmi), 51.6 deg	No direct capability—requires orbital plane change
  Sun-Synchronous Orbit: 800 km (432 nmi), 98.6 deg	?	?	?
  GTO: 5500×35,786 km (2970×19,323 nmi), 25 deg	2500 kg (5500 lbm)	6600 kg (14,000 lbm)	8000 kg (17,600 lbm)
  Geostationary Orbit	1000 kg (2200 lbm)	4000 kg (8800 lbm)	5000 kg (11,000 lbm)

• Payload Compartment

  Max Payload Diameter: A3: 3821 mm (150.4 in) | A5: 3707 mm or 4357 mm (145.9 or 171.5 in)
  Max Cylinder Length: A3: 4166 mm (164.0 in) | A5: 3936 mm or 4918 mm (155.0 or 193.6 in)
  Maximim Cone Length: A3: 5468 mm (215.3 in) | A5: 3814 mm or 6577 mm (150.2 or 258.9 in)

• Dimensions

  Length:

  Angara Universal Model: 25 m (82 ft)

  Diameter: Angara Universal Model:  2.9 m (9.5 ft)

International Launch Services

Russia

Launch Price

No data available

• Performance Summary

  	Angara 1.1	Angara 1.2
  200 km (108 nmi), 63 deg	2000 kg (4400 lbm)	3700 kg (8160 lbm)
  200 km (108 nmi), 90 deg	1650 kg (3640 lbm)	3200 kg (7060 lbm)
  Space Station Orbit: 407 km (220 nmi), 51.6 deg	No direct capability—requires orbital plane change
  Sun-Synchronous Orbit: 800 km (432 nmi), 98.6 deg	?	?
  GTO	No capability	No capability
  Geostationary Orbit	No capability	No capability

• Payload Compartment

  Max Payload Diameter: 2100 x 2380 mm (82.7 x 93.7 in)
  Max Cylinder Length: 3711 mm (146.1 in)
  Maximim Cone Length: 2504 mm (98.6 in)

• Dimensions

  Length:

  6.735 m (22.1 ft)

  Diameter:

United Launch Alliance

United States

Launch Price

Please contact ULA.

• Performance Summary

  Total Orbital Flights: 85
  Launch Vehicle Successes: 85

• Payload Compartment

  Max Payload Diameter: LPF and EPF: 3750 mm (147.6 in.); 5-m Fairing: 4572 mm (180.0 in.)
  Max Cylinder Length: LPF: 4100 mm (161.5 in.); EPF: 5015 mm (197.5 in.); 5-m Short: 4888 mm (192.5 in.); 5-m Medium: 7631 mm (300.5 in.)
  Maximim Cone Length: LPF and EPF: 5296 mm (208.5 in.); 5-m Fairing: 5296 mm (208.4 in.)

• Dimensions

  Length:

  Atlas V 401	Atlas V 411	Atlas V 421	Atlas V 431	Atlas V Starliner	Atlas V 501	Atlas V 511	Atlas V 521	Atlas V 531	Atlas V 541	Atlas V 551
  59 m	59 m	59 m	59 m	52.1 m	61 m	61 m	61 m	61 m	61 m	61 m
  190 ft	190 ft	190 ft	190 ft	171 ft	196 ft	196 ft	196 ft	196 ft	196 ft	196 ft

  Diameter:

  Atlas V 401	Atlas V 411	Atlas V 421	Atlas V 431	Atlas V Starliner	Atlas V 501	Atlas V 511	Atlas V 521	Atlas V 531	Atlas V 541	Atlas V 551
  3.1 m	3.1 m	3.1 m	59 m	3.1 m	3.1 m	3.1 m	3.1 m	3.1 m	3.1 m	3.1 m
  10 ft	10 ft	190 ft	190 ft	10 ft	10 ft	10 ft	10 ft	10 ft	10 ft	10 ft

Space Exploration Technologies

United States

Launch Price

Falcon 9: $62 million plus range and payload specific costs (SpaceX, 2020)

• Performance Summary

  	Falcon 9
  200 km (108 nmi) at 28.5° 200 km (108 nmi) at 90°	22,800 kg
  Space Station orbit: 407 km (220 nmi), 51.6° Sun-synchronous orbit: 800 km (432 nmi), 98.6°	22,800 kg (50,265 lb)
  GTO: 108 ´ 35,786 km (100 nmi ´ 19,323), 27°	8,300 kg (18,300 lb)
  Mars	4,020 kg (8860 lb)
  Pluto

  * Performance represents max capability on fully expendable vehicle

  
  
  

• Payload Compartment

  Max Payload Diameter: 4600 mm (15.1 ft)
  Max Cylinder Length: 1100 mm (36.1 ft)
  Maximim Cone Length: 2794 mm (60 in.)

• Dimensions

  Length: Falcon 9
  70 m / 230 ft (including both stages, interstage, and fairing)
  
  

  
  
  Diameter: Falcon 9
  3.66 m / 12 ft