C-141 Starlifter vs VC-25 "Air Force One"

The C-141 Starlifter and the VC-25 "Air Force One" are both Military Transport Aircraft, manufactured by Lockheed and Boeing respectively. Top speed is 805 km/h for the C-141 Starlifter vs 1,014 km/h for the VC-25 "Air Force One". The C-141 Starlifter has an operational range of 4,723 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 12,497 m for the C-141 Starlifter. At 377,842 kg MTOW, the VC-25 "Air Force One" is 2.6x the C-141 Starlifter's 146,556 kg. The C-141 Starlifter has been produced in 285 units vs 2 for the VC-25 "Air Force One". Unit cost is $40M for the C-141 Starlifter vs $325M for the VC-25 "Air Force One". The C-141 Starlifter first flew 26 years before the VC-25 "Air Force One" (1963 vs 1989).

American military transport aircraft, pivotal during the Vietnam War, chiefly used for strategic airlift missions.
Lockheed C-141 Starlifter Transport profile drawing
Origin country πŸ‡ΊπŸ‡Έ United States
Category Military Transport Aircraft
Manufacturer Lockheed
First flight 17 December 1963
Year introduced 1965
Number produced 285 units
Average unit price $40 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 300.0 mΒ² β—‰
Wingspan 49.0 m β—‰
Height 12.0 m β—‰
Length 51.3 m β—‰
Maximum speed 805 km/h β—‰
Operational range 4,723 km β—‰
Service ceiling 12,497 m β—‰
Max. takeoff weight 146,556 kg β—‰
Empty weight 65,540 kg β—‰
Total thrust 4 x 2,296 kgf 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-141 Starlifter 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-141 Starlifter's 805 km/h, a difference of 209 km/h.
Which has longer range, the C-141 Starlifter or VC-25 "Air Force One"?
The VC-25 "Air Force One" has a longer range at 12,600 km compared to the C-141 Starlifter's 4,723 km.
Which can fly higher, the C-141 Starlifter 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-141 Starlifter's 12,497 meters (41,000 ft).
Which is heavier, the C-141 Starlifter 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-141 Starlifter's 146,556 kg.
Which is larger, the C-141 Starlifter or VC-25 "Air Force One"?
The VC-25 "Air Force One" is longer at 70.6 meters compared to the C-141 Starlifter's 51.3 meters.
Which is more expensive, the C-141 Starlifter 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-141 Starlifter at $40 million.
Which entered service first, the C-141 Starlifter or VC-25 "Air Force One"?
The C-141 Starlifter entered service first in 1965, 25 years before the VC-25 "Air Force One" which entered service in 1990.
Which has been built in greater numbers, the C-141 Starlifter or VC-25 "Air Force One"?
The C-141 Starlifter has been produced in greater numbers with 285 units compared to 2 units of the VC-25 "Air Force One".