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Minotaur-C 3110
Photo: NASA/Richard Nielsen, VAFB · Wikimedia Commons · Public domain
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Minotaur-C3110

Military Space Launch Vehicles · United States · 1994
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Minotaur-C3110

Minotaur-C 3110
Minotaur-C 3110 Photo: NASA/Richard Nielsen, VAFB · Wikimedia Commons · Public domain
* Absolute score — assessed within category · no era adjustment
Payload Capacity
30
Reliability
45
Cost-Efficiency
50
Responsiveness / Cadence
20
Reusability
0
Orbit Versatility
40
Precision
55
Technology
50
Strategic Value
35
Human-Rating
0
Origin United States
CategoryMilitary Space Launch Vehicles
EraPost-Cold War
In service1994–2017
Operators1 countries
Quantity10
Data Quality82%
33
Military Space Launch Vehicles MASS Rating
41/53
Post-Cold War
181/296
All-Time
Military Space Launch Vehicles · 10 axes scored
Payload Capacity
30
Reliability
45
Cost-Efficiency
50
Responsiveness / Cadence
20
Reusability
0
Orbit Versatility
40
Precision
55
Technology
50
Strategic Value
35
Human-Rating
0
ⓘ Regardless of era, the same scoring system applies to all units in the military space launch vehicles category.
01 / Overview
Minotaur-C 3110
Production
1994–2017
Quantity
10
Unit Price (current)
$52.5M↗ 31% inflation · 2017→2025
Original Price
$40.0M (2017)
Operators
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
MILITARY SPACE LAUNCH VEHICLES · POST-COLD WAR
41
PERFORMANCE/PRICE
40
UNIT COST (2025 USD)
$52.5M
Original: $40.0M (2017)
Inflation: +%31
33
military space launch vehicles category
ⓘ Performance/Price and MASS score are computed across all units in the military space launch vehicles category, regardless of era.
02 / Specs & Design
◎General6MOD.6
  • Vehicle TypeSmall-lift launch vehicle
  • First Flight1994
  • ManufacturerOrbital Sciences Corporation (1994–2015), Orbital ATK (2015–2018), Northrop Grumman (2018–present)
  • Stages4
  • StatusRetired
  • In ServiceNo
◈Performance7MOD.7
  • Payload to LEO1,458 kg
  • Payload to SSO1,054 kg
  • Liftoff Thrust1,606.6
  • Liftoff Mass73 t
  • Height27.9 m
  • Diameter2.35 m
  • Success Rate7
▣Propulsion5MOD.5
  • First-Stage PropellantHTPB / Aluminum
  • First-Stage Engines1
  • ReusableNo
  • Human-RatedNo
  • Total Launches10
◇Cost1MOD.1
  • Cost per Launch40,000,000 USD
03 / History
SERVICE LIFESPANStill in Service
  1. 1994Production started
  2. 2017Production ended
32
years in service
23
years in production
10
units produced
1
countries operating
ⓘ The producing country still actively operates it.
04 / Variants
▚ WEAPON FAMILY
Minotaur-C 1994
Minotaur-C 3110 1994
05 / Operators
Operator Countries1country
📚 Sources
📖 ENCYCLOPEDIA Browse the Military Space Launch Vehicles entry →