Delta IV Heavy

ULA Delta IV Heavy 2004 - Hero viewULA Delta IV Heavy 2004 - Top View viewULA Delta IV Heavy 2004 - Profile viewULA Delta IV Heavy 2004 - Bottom View viewULA Delta IV Heavy 2004 - Attach viewULA Delta IV Heavy 2004 - Dcss viewULA Delta IV Heavy 2004 - Fairing viewULA Delta IV Heavy 2004 - Lh2 Tank viewULA Delta IV Heavy 2004 - Thermal Foam viewULA Delta IV Heavy 2004 - Rl10 viewULA Delta IV Heavy 2004 - Rs68a viewULA Delta IV Heavy 2004 - Separation Mechanism view
Hero
Record holder

The most powerful American rocket before Falcon Heavy. Delta IV Heavy launched the Parker Solar Probe, the Orion EFT-1 test flight, and numerous classified national security payloads. Its distinctive fireball at ignition, caused by excess hydrogen burning off, made it one of the most visually dramatic rockets ever launched.

History

Delta IV Heavy used three Common Booster Cores, each powered by an Aerojet Rocketdyne RS-68A engine burning liquid hydrogen and liquid oxygen. It was the only American heavy-lift vehicle available for the most critical national security payloads and high-energy interplanetary missions.

The rocket''s signature visual feature was a fireball that engulfed the base of the vehicle at ignition, caused by gaseous hydrogen burning off before the engines reached full thrust. This looked alarming but was a normal part of the launch sequence.

Delta IV Heavy made its final flight on April 9, 2024, closing out the Delta rocket family after six decades. Its retirement transferred heavy-lift responsibilities to SpaceX''s Falcon Heavy and ULA''s Vulcan Centaur.

Timeline

2004First flight
20242024, closing out the Delta rocket family after six decades

Launch Heritage

Operational StatusRetired
Total Launches15/16 (94%)
Service Period2004-2024
DesignerBoeing / ULA
Mission TypeNational security / Science
ReusabilityExpendable
Cost Per Launch$350M
Orbit TypeLEO
Target BodyEarth
Production Total16
Notable Missions
  • Parker Solar Probe
  • Orion EFT-1
  • NROL missions

Technical Specifications

PropulsionLiquid (LH2/LOX)
Height236.2 ft
Length236.2 ft
Diameter/Wingspan16.4 ft
Gross Mass1,615,986 lbs

Propulsion

Engine ModelRS-68A (3 Common Booster Cores) + RL10B-2 (upper stage)
Engine Count4
Engine ManufacturerAerojet Rocketdyne
Thrust9420 kN
Specific Impulse414 s
PropellantLH2/LOX
Stages2
Boosters2

Performance

Payload to LEO28,790 kg
Payload to GTO14,220 kg

Dimensions

Height (m)71.6 m
Diameter (m)5.13 m
Length (m)71.6 m

Mass

Empty Mass (kg)30,000 kg
Gross Mass (kg)733,000 kg

Mission

Mission Duration16 launches (2004-2024), 15 successes, retired
Missions Flown16
Success Rate15/16
ReusableNo

Power & Systems

AvionicsRIFCA (Redundant Inertial Flight Control Assembly)
Communication BandS-band telemetry, C-band tracking

Source: ULA

Tags

Designed by Boeing / ULA

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