Delta IV Heavy

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Delta IV Heavy
Delta IV launch 2013-08-28.jpg
Delta IV Heavy launches from Vandenberg AFB
Function Orbital launch vehicle
Manufacturer United Launch Alliance
Country of origin United States
Cost per launch (2014) $375 million[1]
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
28,790 kg (63,470 lb)
Payload to
GTO
14,220 kg (31,350 lb)
Associated rockets
Family Delta IV
Launch history
Status Active
Launch sites SLC-37B, Cape Canaveral

SLC-6Vandenberg AFB

Total launches 7
Successes 6
Partial failures 1
First flight December 21, 2004
Boosters (CBC)
No boosters 2
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)[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 sec
Vacuum: 412 sec
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 sec
Vacuum: 412 sec
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 1,125 seconds
Fuel LH2/LOX

The Delta IV Heavy (Delta 9250H) is an expendable rocket, the largest type of the Delta IV family, and the world's highest capacity rocket currently operating.[4] It was first launched in 2004.[5]

The Delta IV Heavy uses two hydrogen-fueled Common Booster Cores as boosters instead of the solid Graphite-Epoxy 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 while the boosters continue to operate at full thrust. 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 first launch of the Delta IV Heavy in 2004 carried a boilerplate payload, and was a partial failure. Cavitation in the liquid oxygen propellant lines caused shutdown of both boosters and the core CBC several 8 and 9 seconds early, respectively, resulting in a lower staging velocity which the second stage was unable to compensate for. The payload was left in a lower than intended orbit.[6] Its first operational payload was the DSP-23 satellite, successfully launched in 2007.

Capacity of the Delta IV Heavy:

The Heavy's total mass at launch is approximately 733,000 kg.

The Orion Multi-Purpose Crew Vehicle is planned for an uncrewed test flight, known as EFT-1, aboard a Delta IV Heavy rocket in December 2014.[9]

Comparable vehicles[edit]

References[edit]

  1. ^ "Solar Probe Plus, NASA’s ‘Mission to the Fires of Hell,’ Trading Atlas 5 for Bigger Launch Vehicle". Space Now. Retrieved July 26, 2014. 
  2. ^ "Delta IV Heavy". Spaceflight 101. Retrieved July 2014. 
  3. ^ a b "Delta IV Payload Planner's Guide, June 2013". United Launch Alliance. Retrieved July 2014. 
  4. ^ "Mission Status Center". SpaceflightNow. Retrieved July 2014. "The ULA Delta 4-Heavy is currently the world’s largest rocket, providing the nation with reliable, proven, heavy lift capability for our country's national security payloads from both the east and west coasts." 
  5. ^ "Boeing Delta IV Heavy Achieves Major Test Objectives in First Flight", Boeing, 2004, accessed March 22, 2012
  6. ^ "Delta 4-Heavy investigation identifies rocket's problem". Spaceflight Now. Retrieved July 2014. 
  7. ^ a b c "Delta IV Launch Services User's Guide". United Launch Alliance. June 2013. pp. 2–10,5–3. 
  8. ^ "Delta IV Data Sheet". Space Launch Report. Retrieved July 2014. 
  9. ^ Bergin, Chris (2012-01-18). "EFT-1 set to receive Spring, 2014 launch date after contract negotiations". NASASpaceFlight.com. Retrieved 21 July 2012.