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Lockheed XH-51
Photo: US Army · Wikimedia Commons · Public domain Use of this image does not imply endorsement by the U.S. Department of Defense (DoD).
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LockheedXH-51

Utility / Transport Helicopters · United States · 1962
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LockheedXH-51

Lockheed XH-51
Lockheed XH-51 Photo: US Army · Wikimedia Commons · Public domain Use of this image does not imply endorsement by the U.S. Department of Defense (DoD).
* Absolute score — assessed within category · no era adjustment
Payload / Capacity
30
Range
25
Versatility
45
Reliability
50
Speed
60
Survivability
35
Hot-and-High Performance
40
Maintainability
55
Technology
80
Cost-Effectiveness
30
Origin United States
CategoryUtility / Transport Helicopters
EraEarly Cold War
In service1962–1964
Operators1 countries
Quantity3
Data Quality84%
43
Utility / Transport Helicopters MASS Rating
26/42
Early Cold War
176/208
All-Time
Utility / Transport Helicopters · 10 axes scored
Payload / Capacity
30
Range
25
Versatility
45
Reliability
50
Speed
60
Survivability
35
Hot-and-High Performance
40
Maintainability
55
Technology
80
Cost-Effectiveness
30
ⓘ Regardless of era, the same scoring system applies to all units in the utility / transport helicopters category.
01 / Overview
Lockheed XH-51
Production
1962–1964
Quantity
3
Operators
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
UTILITY / TRANSPORT HELICOPTERS · EARLY COLD WAR
26
PERFORMANCE/PRICE
25
UNIT COST (2025 USD)
—
43
utility / transport helicopters category
ⓘ Performance/Price and MASS score are computed across all units in the utility / transport helicopters category, regardless of era.
02 / Specs & Design
◎General5MOD.5
  • First Flight1962
  • Crew1
  • Passengers3
  • Primary Roleexperimental rigid-rotor research helicopter
  • In ServiceYes
◈Powerplant6MOD.6
  • Engine TypePratt & Whitney Canada PT6B-9
  • Number of Engines1
  • Engine Power (each)410 kW
  • Rotor Configurationrigid rotor
  • Main Rotor Blades4
  • Anti-Torque Typetail rotor
▣Performance2MOD.2
  • Top Speed280.001 km/h
  • Cruise Speed257.472 km/h
◇Dimensions & Weights2MOD.2
  • Fuselage Length12.192 m
  • Height2.5 m
◆Armament & Mission5MOD.5
▲Production2MOD.2
  • Total Built3
  • Variants4
◎Service History3MOD.3
  • Production Start1962
  • Production End1964
  • Operational StatusRetired
03 / History
SERVICE LIFESPANRetired
  1. 1962Production started
  2. 1964Production ended
64
years in service
2
years in production
3
units produced
0
countries operating
ⓘ The producing country no longer actively operates it. 1 countries retired it.
04 / Operators
Operator Countries1country
📚 Sources
📖 ENCYCLOPEDIA Browse the Utility / Transport Helicopters entry →