Summary

variant of the Delta IV space launch vehicle

Delta IV Heavy

Delta IV Heavy launches from Vandenberg
Function	Orbital heavy-lift launch vehicle
Manufacturer	United Launch Alliance
Country of origin	United States
Cost per launch	US$350 million [1] NRO: US$440 million
Cost per year	2018
Size
Height	72 m (236 ft)
Diameter	5 m (16 ft)
Width	15 m (49 ft)
Mass	733,000 kg (1,616,000 lb)
Stages	2+
Capacity
Payload to LEO
Mass	28,790 kg (63,470 lb)
Payload to GTO
Mass	14,220 kg (31,350 lb)
Associated rockets
Family	Delta IV
Comparable	Ariane 5 Falcon Heavy Long March 5 Proton-M
Launch history
Status	Active
Launch sites	Cape Canaveral, SLC-37B VAFB, SLC-6
Total launches	11
Success(es)	10
Partial failure(s)	1
First flight	21 December 2004 (USA-181)
Last flight	19 January 2019 (NROL-71)
Notable payloads	EFT-1 NRO classified payloads Kennen Orion Parker Solar Probe
Boosters (CBC)
No. boosters	2
Length	40.8 m (134 ft)
Diameter	5.1 m (17 ft)
Empty mass	26,000 kg (57,000 lb)
Gross mass	226,400 kg (499,100 lb)
Propellant mass	200,400 kg (441,800 lb) [2]
Engines	1 RS-68A
Thrust	3,140 kN (710,000 lbf)
Total thrust	6,280 kN (1,410,000 lbf)
Specific impulse	Sea level: 360 s (3.5 km/s) Vacuum: 412 s (4.04 km/s)
Burn time	242 seconds [3]
Fuel	LH2 / LOX
First stage (CBC)
Length	40.8 m (134 ft)
Diameter	5.1 m (17 ft)
Gross mass	226,400 kg (499,100 lb)
Propellant mass	200,400 kg (441,800 lb)
Engines	1 RS-68A
Thrust	3,140 kN (710,000 lbf)
Specific impulse	Sea level: 360 s (3.5 km/s) Vacuum: 412 s (4.04 km/s)
Burn time	328 seconds
Fuel	LH2 / LOX
Second stage (DCSS)
Length	13.7 m (45 ft)
Diameter	5.1 m (17 ft)
Gross mass	30,700 kg (67,700 lb)
Propellant mass	27,220 kg (60,010 lb)
Engines	1 RL10-B-2
Thrust	110 kN (25,000 lbf)
Specific impulse	462 s (4.53 km/s)
Burn time	1125 seconds
Fuel	LH2 / LOX

The Delta IV Heavy (Delta 9250H) is an expendable heavy-lift launch vehicle, the largest type of the Delta IV family and the world's second highest-capacity rocket in operation, behind SpaceX's Falcon Heavy rocket (in expendable configuration).^[4][5] It is manufactured by United Launch Alliance and was first launched in 2004.^[6]

The Delta IV Heavy consists of a central Common Booster Core (CBC), with two additional CBCs as liquid rocket boosters instead of the GEM-60 solid rocket motors used by the Delta IV Medium+ versions. At lift off, all three cores operate at full thrust, and 44 seconds later the center core throttles down to 55% to conserve fuel until booster separation. The boosters burn out at 242 seconds after launch and are separated as the core booster throttles back up to full thrust. The core burns out 86 seconds later, and the second stage completes the ascent to orbit.^[3]

The rocket uses three RS-68 engines, one in the central core and one in each booster.^[7]

History

Delta IV Heavy for Exploration Flight Test-1 (EFT-1), in 2014.

The Delta IV line of rockets was developed by McDonnell Douglas, later United Launch Alliance. The Delta IV Heavy is the most powerful member of the line, which also includes the smaller Delta IV Medium.^[8] The Delta IV Heavy can lift 28,370 kg (62,550 lb) to low Earth orbit and 13,810 kg (30,450 lb) to geostationary transfer orbit.^[8] It is an all liquid-fueled rocket, consisting of an upper stage, one main booster and two strap-on boosters.^[8]

The first launch of the Delta IV Heavy in 2004 carried a boilerplate payload and failed to reach intended orbit. Cavitation in the liquid-oxygen propellant lines caused shutdown of both boosters eight seconds early, and the core engine nine seconds early; this resulted in a lower staging velocity for which the second stage was unable to compensate. The payload was left in a lower than intended orbit.^[9] Its first operational payload was the DSP-23 satellite, successfully launched in 2007; it was then used to launch a further five visual and electronic reconnaissance satellites for the National Reconnaissance Office through 2013.

In December 2014, the Delta IV Heavy was used to launch an uncrewed test flight of the Orion spacecraft, designated Exploration Flight Test 1 (EFT-1). After several delays, the mission was successfully launched at 12:05 UTC on 5 December 2014.^[10]

Capability

Capacity of the Delta IV Heavy:

• Low Earth orbit (LEO), 200 km × 28.7°: 28,790 kg (63,470 lb) ^[11]
• Low Earth orbit (ISS), 407 km × 51.6°: 25,980 kg (57,280 lb) ^[12]
• Geosynchronous transfer orbit (GTO): 14,220 kg (31,350 lb) ^[11]
• Geosynchronous orbit (GEO): 6,750 kg (14,880 lb) ^[11]
• Lunar transfer orbit (LTO): 10,000 kg (22,000 lb)
• Mars transfer orbit: 8,000 kg (18,000 lb) ^[13]

The Delta IV Heavy's total mass at launch is approximately 733,000 kg (1,616,000 lb) and produce around 952,000 kg (2,099,000 lb) of thrust to power the rocket skyward at liftoff.^[14]

Launch history

Upcoming launches

The following missions have been announced by the National Reconnaissance Office.^[17][18] As of October 2020, these are the final five missions.^[19]

For these missions including modifications, ULA has been awarded US$2.2 billion, or US$440 million per launch.^[20]

Comparable vehicles

See also

• Heavy-lift launch vehicle
• Comparison of orbital launch systems
• Comparison of orbital rocket engines
• Comparison of space station cargo vehicles
• National Launch System, (1991–1993) study

References

External links

• Delta IV Booster Integration Another Step Toward First Orion Flight