C-130 Hercules vs VC-25 "Air Force One"

The C-130 Hercules and the VC-25 "Air Force One" are both Military Transport Aircraft, manufactured by Lockheed and Boeing respectively. Top speed is 593 km/h for the C-130 Hercules vs 1,014 km/h for the VC-25 "Air Force One". The C-130 Hercules has an operational range of 3,800 km vs 12,600 km for the VC-25 "Air Force One". The VC-25 "Air Force One" operates at altitudes up to 13,746 m compared to 10,058 m for the C-130 Hercules. At 377,842 kg MTOW, the VC-25 "Air Force One" is 5.4x the C-130 Hercules's 70,307 kg. The C-130 Hercules has been produced in 2,500 units vs 2 for the VC-25 "Air Force One". Unit cost is $68M for the C-130 Hercules vs $325M for the VC-25 "Air Force One". The C-130 Hercules first flew 35 years before the VC-25 "Air Force One" (1954 vs 1989).

American military transport aircraft, known for significant roles in Vietnam War and Desert Storm, extensively used for various cargo missions.
Lockheed C-130 Hercules Transport profile drawing
Origin country πŸ‡ΊπŸ‡Έ United States
Category Military Transport Aircraft
Manufacturer Lockheed
First flight 23 August 1954
Year introduced 1956
Number produced 2500 units
Average unit price $68 million
American presidential transport aircraft, deployed since the mid-1980s, known for brass-bound luxury and sophisticated communications.
Boeing VC-25 "Air Force One" Transport profile drawing
Origin country πŸ‡ΊπŸ‡Έ United States
Category Military Transport Aircraft
Manufacturer Boeing
First flight 1 September 1989
Year introduced 1990
Number produced 2 units
Average unit price $325 million
Wing area 162.0 mΒ² β—‰
Wingspan 40.4 m β—‰
Height 11.7 m β—‰
Length 29.8 m β—‰
Maximum speed 593 km/h β—‰
Operational range 3,800 km β—‰
Service ceiling 10,058 m β—‰
Max. takeoff weight 70,307 kg β—‰
Empty weight 35,800 kg β—‰
Total thrust 4 x 915 kW β—‰
Wing area 511.0 mΒ² β—‰
Wingspan 59.6 m β—‰
Height 19.3 m β—‰
Length 70.6 m β—‰
Maximum speed 1014 km/h β—‰
Operational range 12,600 km β—‰
Service ceiling 13,746 m β—‰
Max. takeoff weight 377,842 kg β—‰
Empty weight 173,726 kg β—‰
Total thrust 4 x 6,430 kgf β—‰

Performance Radar Chart

Frequently Asked Questions

Which is faster, the C-130 Hercules or VC-25 "Air Force One"?
The VC-25 "Air Force One" is faster with a maximum speed of 1,014 km/h compared to the C-130 Hercules's 593 km/h, a difference of 421 km/h.
Which has longer range, the C-130 Hercules or VC-25 "Air Force One"?
The VC-25 "Air Force One" has a longer range at 12,600 km compared to the C-130 Hercules's 3,800 km.
Which can fly higher, the C-130 Hercules or VC-25 "Air Force One"?
The VC-25 "Air Force One" has a higher service ceiling at 13,746 meters (45,098 ft) compared to the C-130 Hercules's 10,058 meters (32,998 ft).
Which is heavier, the C-130 Hercules or VC-25 "Air Force One"?
The VC-25 "Air Force One" has a higher maximum takeoff weight at 377,842 kg compared to the C-130 Hercules's 70,307 kg.
Which is larger, the C-130 Hercules or VC-25 "Air Force One"?
The VC-25 "Air Force One" is longer at 70.6 meters compared to the C-130 Hercules's 29.8 meters.
Which is more expensive, the C-130 Hercules or VC-25 "Air Force One"?
The VC-25 "Air Force One" is more expensive at approximately $325 million per unit compared to the C-130 Hercules at $68 million.
Which entered service first, the C-130 Hercules or VC-25 "Air Force One"?
The C-130 Hercules entered service first in 1956, 34 years before the VC-25 "Air Force One" which entered service in 1990.
Which has been built in greater numbers, the C-130 Hercules or VC-25 "Air Force One"?
The C-130 Hercules has been produced in greater numbers with 2,500 units compared to 2 units of the VC-25 "Air Force One".