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Delta IV

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Delta IV
NameDelta IV
CaptionA Delta IV Heavy lifting off from Space Launch Complex 37
FunctionExpendable launch system
ManufacturerUnited Launch Alliance (ULA)
Country originUnited States
Height63–72 m (207–236 ft)
Diameter5 m (16 ft)
Mass249,500–733,400 kg (550,100–1,616,900 lb)
Capacity LEO8,210–28,790 kg (18,100–63,470 lb)
Capacity GTO4,440–14,220 kg (9,790–31,350 lb)
StatusRetired
Launches45
Success44
First2002-11-20
Last2024-04-09

Delta IV. It was a family of expendable launch systems developed for the United States Air Force's Evolved Expendable Launch Vehicle (EELV) program and manufactured by United Launch Alliance. The rocket series was renowned for its powerful Delta IV Heavy configuration, which served as a critical national security asset for the U.S. Space Force and National Reconnaissance Office, while also launching significant scientific missions for NASA. Its final flight in 2024 concluded over two decades of service, marking the end of an era for American heavy-lift rocketry.

Overview

The Delta IV family was conceived as a modern successor to earlier Delta II and Delta III rockets, designed to provide assured access to space for critical United States Department of Defense payloads. Its core design centered on the Common Booster Core (CBC), a modular liquid-fueled rocket stage powered by a single RS-68 engine burning liquid hydrogen and liquid oxygen. Operated primarily from Cape Canaveral Space Force Station and Vandenberg Space Force Base, the vehicle maintained an exceptional reliability record throughout its career. The program was a cornerstone of the American aerospace industry, involving major contractors like Boeing and utilizing facilities such as the Decatur assembly plant.

Development and design

Development began in the 1990s under the Evolved Expendable Launch Vehicle program, a United States Air Force initiative to reduce launch costs and improve reliability. The design, led by Boeing Integrated Defense Systems, introduced the innovative Common Booster Core and the powerful RS-68 engine, developed by Rocketdyne. A key feature was the use of a Composite Overwrapped Pressure Vessel for helium storage and extensive aluminum-lithium alloy in tank construction. The upper stage was a derivative of the Delta II's Delta-K stage, upgraded with a Pratt & Whitney RL10B-2 engine featuring an extendable carbon-carbon nozzle. The rocket's Inertial Navigation System and avionics were supplied by Honeywell.

Variants

The family comprised five main variants, differentiated by the number of Common Booster Cores and the size of the payload fairing. The Delta IV Medium featured a single CBC with either a 4-meter or 5-meter fairing. The Delta IV Medium+ configurations added up to four Graphite-Epoxy Motor solid rocket boosters, provided by Northrop Grumman, to augment thrust at liftoff. The most capable variant was the Delta IV Heavy, which utilized three CBCs strapped together to form a triple-core vehicle; this configuration was comparable in lift capacity to the Titan IV and was used for the most demanding missions. All variants shared the same Delta Cryogenic Second Stage powered by the RL10.

Launch history

The maiden flight, a Delta IV Medium, occurred on November 20, 2002, from Space Launch Complex 37 at Cape Canaveral Space Force Station, carrying the Eutelsat W5 communications satellite. The inaugural Delta IV Heavy launch in 2004 experienced a partial failure due to premature booster shutdown. Subsequent Heavy flights, however, achieved complete success, launching vital payloads for the National Reconnaissance Office such as the KH-11 Kennen satellites and critical missions for NASA including the Orion spacecraft's Exploration Flight Test 1. The only total failure was a Medium+ mission in 2024, attributed to a liquid hydrogen leak. The final flight, a Heavy, successfully deployed a NROL-70 payload in April 2024.

Retirement and legacy

The vehicle was retired as part of a strategic transition by United Launch Alliance to its next-generation Vulcan Centaur rocket, which incorporates advanced technologies like the BE-4 engine from Blue Origin. Its legacy is defined by unparalleled mission assurance for American national security space launches and key contributions to exploration, such as launching the Parker Solar Probe. The Delta IV Heavy's dramatic orange foam insulation and fiery hydrogen flare at liftoff became iconic in launch photography. Its retirement concludes the entire Delta (rocket family) lineage, which began in 1960 with the Thor-Delta and included historic missions like the launch of Syncom and the Mars Pathfinder.

Category:Expendable launch systems Category:Delta rockets Category:2002 in spaceflight