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 ▾
Mercury-Redstone Launch Vehicle
Photo: NASA · Wikimedia Commons · Public domain
REC // INTEL FEED

Mercury-RedstoneLaunchVehicle

Military Space Launch Vehicles · United States · 1959
ADD TO COMPARE

Mercury-RedstoneLaunchVehicle

Mercury-Redstone Launch Vehicle
Mercury-Redstone Launch Vehicle Photo: NASA · Wikimedia Commons · Public domain
* Absolute score — assessed within category · no era adjustment
Payload Capacity
30
Reliability
55
Cost-Efficiency
45
Responsiveness / Cadence
50
Reusability
5
Orbit Versatility
10
Precision
40
Technology
45
Strategic Value
60
Human-Rating
70
Origin United States
ManufacturerStellantis North America
CategoryMilitary Space Launch Vehicles
EraEarly Cold War
In service1959–1961
Operators1 countries
Quantity6
Data Quality84%
40
Military Space Launch Vehicles MASS Rating
7/53
Early Cold War
141/296
All-Time
Military Space Launch Vehicles · 10 axes scored
Payload Capacity
30
Reliability
55
Cost-Efficiency
45
Responsiveness / Cadence
50
Reusability
5
Orbit Versatility
10
Precision
40
Technology
45
Strategic Value
60
Human-Rating
70
ⓘ Regardless of era, the same scoring system applies to all units in the military space launch vehicles category.
01 / Overview
Mercury-Redstone Launch Vehicle
Prime contractor
Production
1959–1961
Quantity
6
Operators
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
MILITARY SPACE LAUNCH VEHICLES · EARLY COLD WAR
7
PERFORMANCE/PRICE
68
UNIT COST (2025 USD)
—
40
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 Typesuborbital launch vehicle
  • First Flight1960
  • ManufacturerChrysler Corporation
  • Stages1
  • StatusRetired
  • In ServiceYes
◈Performance5MOD.5
  • Liftoff Thrust347
  • Liftoff Mass30 t
  • Height25.41 m
  • Diameter1.77 m
  • Success Rate5
▣Propulsion5MOD.5
  • First-Stage PropellantLOX/ethyl alcohol
  • First-Stage Engines1
  • ReusableNo
  • Human-RatedYes
  • Total Launches6
03 / History
SERVICE LIFESPANRetired
  1. 1959Production started
  2. 1960Entered service
  3. 1961Production ended
67
years in service
2
years in production
6
units produced
0
countries operating
ⓘ The producing country no longer actively operates it. 1 countries retired it.
04 / Operators
Operator Countries1country
📖 TERMS ON THIS PAGE1terms
Capable of carrying human passengers, meeting safety and reliability standards for human spaceflight.
These terms are listed automatically because they appear on this page.full encyclopedia →
📚 Sources
📖 ENCYCLOPEDIA Browse the Military Space Launch Vehicles entry →