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AIM-4 Falcon
Photo: Wilson44691 · Wikimedia Commons · CC0
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AIM-4Falcon

Medium-Range AAM (MRAAM / BVR) · United States · 1956
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AIM-4Falcon

AIM-4 Falcon
AIM-4 Falcon Photo: Wilson44691 · Wikimedia Commons · CC0
* Absolute score — assessed within category · no era adjustment
Range
30
Seeker / Guidance
40
No-Escape Zone
35
Speed
45
Counter-Measure Resistance
25
Lethality
50
Data-Link
0
Reliability
40
Technology
30
Cost-Effectiveness
55
Origin United States
ManufacturerHughes Aircraft Company
CategoryMedium-Range AAM (MRAAM / BVR)
EraEarly Cold War
In service1956–1988
Operators7 countries
Quantity16,000
Data Quality88%
34
Medium-Range AAM (MRAAM / BVR) MASS Rating
13/22
Early Cold War
53/73
All-Time
Medium-Range AAM (MRAAM / BVR) · 10 axes scored
Range
30
Seeker / Guidance
40
No-Escape Zone
35
Speed
45
Counter-Measure Resistance
25
Lethality
50
Data-Link
0
Reliability
40
Technology
30
Cost-Effectiveness
55
ⓘ Regardless of era, the same scoring system applies to all units in the medium-range aam (mraam / bvr) category.
01 / Overview
AIM-4 Falcon
Prime contractor
Production
1956–1988
Quantity
16,000
Operators
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
MEDIUM-RANGE AAM (MRAAM / BVR) · EARLY COLD WAR
13
PERFORMANCE/PRICE
60
UNIT COST (2025 USD)
—
34
medium-range aam (mraam / bvr) category
ⓘ Performance/Price and MASS score are computed across all units in the medium-range aam (mraam / bvr) category, regardless of era.
02 / Specs & Design
◎General8MOD.8
  • Missile TypeMedium-Range AAM (MRAAM / BVR)
  • Service Entry Year1956
  • DesignerHughes Aircraft
  • Length1.98 m
  • Diameter163 mm
  • Wingspan / Fin Span508 mm
  • Launch Weight68 kg
  • In ServiceYes
◈Guidance8MOD.8
▣Propulsion5MOD.5
  • Propulsion Typesolid fuel rocket
  • Motor Typesolid-propellant rocket motor
  • Boost StageNo
  • Two-StageNo
  • Fuel / Propellantsolid
◇Performance8MOD.8
  • Minimum Range0.5 km
  • Maximum Range9.7 km
  • Top Speed1,029 m/s
  • Top Speed (Mach)3 Mach
  • Cruise Altitude18,000 m
  • Flight Profiletail-chase and head-on intercepts
  • Maximum G30
  • HypersonicNo
◆Warhead6MOD.6
▤Launch Platform6MOD.6
⬢Production4MOD.4
  • Total Production16,000
  • Operators7
  • Variants10
  • Production Start1,946 year
▲Warhead Detail3MOD.3
  • Detonation Mechanism / Fuzecontact fuze
  • Explosive Filler Weight3.4 kg
  • Explosive Filler Typeliquid nitrogen (coolant)
03 / History
SERVICE LIFESPANStill in Service
  1. 1956Production started
  2. 1958Entered service
  3. 1988Production ended
70
years in service
32
years in production
16,000
units produced
6
countries operating
ⓘ The producing country still actively operates it. 1 countries retired it.
04 / Operators
📖 TERMS ON THIS PAGE2terms
Capability of launching an anti-tank guided missile from an airborne platform, such as a helicopter or aircraft.
A guidance method where a missile uses radar reflections from an external illuminator, typically a ground or airborne radar, to track and intercept a target.
These terms are listed automatically because they appear on this page.full encyclopedia →
📚 Sources
📖 ENCYCLOPEDIA Browse the Medium-Range AAM (MRAAM / BVR) entry →