Delta II

Douglas/Boeing Delta II 1989 - Hero viewDouglas/Boeing Delta II 1989 - Top View viewDouglas/Boeing Delta II 1989 - Profile viewDouglas/Boeing Delta II 1989 - Bottom View viewDouglas/Boeing Delta II 1989 - Fairing viewDouglas/Boeing Delta II 1989 - First Stage viewDouglas/Boeing Delta II 1989 - Gem viewDouglas/Boeing Delta II 1989 - Second Stage viewDouglas/Boeing Delta II 1989 - Gems viewDouglas/Boeing Delta II 1989 - Rs27a viewDouglas/Boeing Delta II 1989 - Sharkteeth viewDouglas/Boeing Delta II 1989 - Star48b view
Hero
Most launched

NASA''s reliable medium-lift workhorse for nearly three decades. Delta II launched the Mars rovers Spirit and Opportunity, the GPS satellite constellation, the Kepler space telescope, and dozens of other missions with a 98.7% success rate.

History

Delta II was the descendant of the Thor intermediate-range ballistic missile, carrying forward a rocket lineage that began in the 1950s. Boeing (through its heritage company Douglas Aircraft) refined the design into one of the most reliable launch vehicles in history.

The rocket''s versatility made it NASA''s preferred launch vehicle for mid-size science missions. It placed the Pathfinder lander and Sojourner rover on Mars, launched the twin Mars Exploration Rovers Spirit and Opportunity, deployed the GPS constellation that revolutionized navigation, and carried the Kepler space telescope to its planet-hunting orbit.

Delta II flew 155 times between 1989 and 2018, with only two failures -- a success rate of 98.7%. Its retirement in 2018, after launching the ICESat-2 Earth observation satellite, ended a rocket family whose lineage spanned six decades and over 400 flights across all Delta variants.

Timeline

1989First flight
2018Delta II flew 155 times between 1989 and 2018, with only two failures -- a success rate of 98.7%

Launch Heritage

Operational StatusRetired
Total Launches153/155 (99%)
Service Period1989-2018
DesignerMcDonnell Douglas / Boeing
Mission TypeSatellite delivery / Science
ReusabilityExpendable
Cost Per Launch$65M
Orbit TypeLEO
Target BodyEarth
Production Total155
Notable Missions
  • Mars Exploration Rovers
  • GPS constellation
  • MESSENGER
  • Kepler

Technical Specifications

PropulsionLiquid (RP-1) + Solid
Height128 ft
Length128 ft
Diameter/Wingspan8 ft
Gross Mass511,472 lbs

Propulsion

Engine ModelRS-27A (first stage) + AJ10-118K (second stage) + Star-48B (optional third)
Engine Count1
Engine ManufacturerRocketdyne / Aerojet
Thrust1054 kN
Specific Impulse302 s
PropellantRP-1/LOX (stage 1) + N2O4/Aerozine-50 (stage 2)
Stages2
Boosters9

Performance

Payload to LEO6,100 kg
Payload to GTO2,170 kg

Dimensions

Height (m)39 m
Diameter (m)2.44 m
Length (m)39 m

Mass

Empty Mass (kg)6,760 kg
Gross Mass (kg)231,870 kg

Mission

Mission Duration155 launches (1989-2018), 153 successes
Missions Flown155
Success Rate153/155
ReusableNo

Power & Systems

AvionicsRS-27A engine controller, redundant inertial guidance
Communication BandS-band, C-band tracking

Source: ULA, NASA

Tags

Designed by McDonnell Douglas / Boeing

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