LATEST Ancient Prototypes of Proxy Warfare: The Economic and Logistical Burden of Roman and Persian Proxy Networks among Arab Tribes and Caucasian Powers
SEARCH
DB ONLINE
EN ▾
Minotaur
Photo: Painter of London E 4 · Wikimedia Commons · CC BY 2.5
REC // INTEL FEED

Minotaur

Military Space Launch Vehicles · United States · 1994
ADD TO COMPARE

Minotaur

Minotaur
Minotaur Photo: Painter of London E 4 · Wikimedia Commons · CC BY 2.5
* 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
ManufacturerOrbital Sciences Corporation, Northrop Grumman Space Systems, Northrop Grumman Innovation Systems
CategoryMilitary Space Launch Vehicles
EraPost-Cold War
In service1994
Operators2 countries
Data Quality83%
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
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
MILITARY SPACE LAUNCH VEHICLES · POST-COLD WAR
41
PERFORMANCE/PRICE
45
UNIT COST (2025 USD)
—
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 Typesolid-fuel launch vehicle
  • First Flight1994
  • ManufacturerNorthrop Grumman
  • Stages4
  • StatusOperational
  • In ServiceYes
◈Performance7MOD.7
  • Payload to LEO580 kg
  • Payload to SSO310 kg
  • Liftoff Thrust1,606.6
  • Liftoff Mass73 t
  • Height27.9 m
  • Diameter2.35 m
  • Success Rate0.7
▣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
32
years in service
2
countries operating
ⓘ The producing country still actively operates it.
04 / Variants
▚ WEAPON FAMILY
Minotaur 1994
// DERIVATIVES
05 / Operators
Operator Countries2country
📚 Sources
📖 ENCYCLOPEDIA Browse the Military Space Launch Vehicles entry →