Vulcan Centaur

Last updated

CH4
  1. 407 km (253 mi) circular orbit at 51.6° inclination
  2. 555 km (345 mi) circular orbit at 98.75° inclination
  3. 20,368 km (12,656 mi) circular orbit at 55° inclination
  4. 36,101 km (22,432 mi) circular orbit at 0° inclination
  5. 1,800 m/s delta-V with 185 km (115 mi) perigee and 35,786 km (22,236 mi) apogee orbit at 27° inclination
  6. 1,203 km (748 mi) perigee and 39,170 km (24,340 mi) apogee orbit at 63.4° inclination
  7. C3: -2 km2/sec2

These capabilities reflect NSSL requirements, plus room for growth. [5] [71]

A Vulcan Centaur with six solid rocket boosters can put 27,200 kilograms into low Earth orbit, nearly as much as the three-core Delta IV Heavy. [72]

Vulcan Centaur launches

2024

Vulcan Centaur
Vulcan logo.svg
CLPS PM-1 Astrobotic-ULA Rollout for Launch (KSC-20240105-PH-JBS01 0067) (cropped).jpg
Vulcan Centaur in VC2S configuration ahead of its maiden flight
Function Heavy-lift launch vehicle
Manufacturer United Launch Alliance
Country of originUnited States
Cost per launchAbout US$100–200 million [1] [2]
Size
HeightStandard: 61.6 m (202 ft)
Long: 67.3 m (221 ft) [3]
Diameter5.4 m (18 ft) [4]
Mass546,700 kg (1,205,300 lb)
Stages2
Capacity
Payload to LEO
Orbital inclination28.7°
Mass27,200 kg (60,000 lb) [5]
Total launches1
Success(es)1
First flight8 January 2024 [7]
Boosters – GEM-63XL
No. boosters0, 2, 4, or 6 [8]
Height22.0 m (865 in)
Diameter1.62 m (63.7 in)
Empty mass4,521 kg (9,966 lb)
Gross mass53,030 kg (116,920 lb)
Propellant mass47,853 kg (105,497 lb)
Maximum thrust2,044 kN (460,000 lbf) each
Specific impulse 280.3 s (2.749 km/s)
Burn time87.3 seconds
Propellant AP / HTPB / Al

Future launches

Future launches are listed chronologically when firm plans are in place. The order of the later launches is much less certain. [75] Launches are expected to take place "no earlier than" (NET) the listed date.

2024

2025

2027

TBD

Potential upgrades

Since 2015, ULA has spoken of several technologies that would improve the Vulcan launch vehicle's capabilities. These include first-stage improvements to make the most expensive components potentially reusable and second-stage improvements to allow the rocket to operate for months in Earth-orbit cislunar space. [97]

Long-endurance upper stages

The ACES upper stage—fueled with liquid oxygen (LOX) and liquid hydrogen (LH2) and powered by up to four rocket engines with the engine type yet to be selected—was a conceptual upgrade to Vulcan's upper stage at the time of the announcement in 2015. This stage could be upgraded to include Integrated Vehicle Fluids technology that would allow the upper stage to function in orbit for weeks instead of hours. The ACES upper stage was cancelled in September 2020, [31] [98] and ULA said the Vulcan second stage would now be the Centaur V upper stage: a larger, more powerful version of the Dual Engine Centaur upper stage used by the Atlas V N22. [19] [97] A senior executive at ULA said the Centaur V design was also heavily influenced by ACES. [99] [72]

However, ULA said in 2021 that it is working to add more value to upper stages by having them perform tasks such as operating as space tugs. CEO Tory Bruno says ULA is working on upper stages with hundreds of times the endurance of those currently in use. [99]

SMART reuse

A method of main engine reuse called Sensible Modular Autonomous Return Technology (SMART) is a proposed upgrade for Vulcan Centaur. In the concept, the booster engines, avionics, and thrust structure detach as a module from the propellant tanks after booster engine cutoff. The engine module then falls through the atmosphere protected by an inflatable heat shield. After parachute deployment, the engine section splashes down, using the heatshield as a raft. [100] ULA estimated this technology could reduce the cost of the first stage propulsion by 90%, and 65% of the total first-stage cost. [32] [100] Although SMART reuse was not initially funded for development, [97] from 2021 the higher launch cadence required to launch the Project Kuiper megaconstellation provided support for the concept's business case. [101] Prior to 2022, ULA intended to catch the engine section using a helicopter. [100]

Vulcan Heavy

In September 2020, ULA announced that they were carefully studying a "Vulcan Heavy" variant with three booster cores. Speculation about a new variant had been rampant for months after an image of a model of that version popped on social media. ULA CEO Tory Bruno later tweeted a clearer image of the model and said it was the subject of ongoing study. [102] [103] [ needs update ]

See also

Related Research Articles

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The Centaur is a family of rocket propelled upper stages that has been in use since 1962. It is currently produced by U.S. launch service provider United Launch Alliance, with one main active version and one version under development. The 3.05 m (10.0 ft) diameter Common Centaur/Centaur III flies as the upper stage of the Atlas V launch vehicle, and the 5.4 m (18 ft) diameter Centaur V has been developed as the upper stage of ULA's new Vulcan rocket. Centaur was the first rocket stage to use liquid hydrogen (LH2) and liquid oxygen (LOX) propellants, a high-energy combination that is ideal for upper stages but has significant handling difficulties.

<span class="mw-page-title-main">Delta IV</span> Retired expendable launch system in the Delta rocket family

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<span class="mw-page-title-main">National Security Space Launch</span> Expendable launch system program of the United States Space Force

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<span class="mw-page-title-main">RL10</span> Liquid fuel cryogenic rocket engine, typically used on rocket upper stages

The RL10 is a liquid-fuel cryogenic rocket engine built in the United States by Aerojet Rocketdyne that burns cryogenic liquid hydrogen and liquid oxygen propellants. Modern versions produce up to 110 kN (24,729 lbf) of thrust per engine in vacuum. Three RL10 versions are in production for the Centaur upper stage of the Atlas V and the DCSS of the Delta IV. Three more versions are in development for the Exploration Upper Stage of the Space Launch System and the Centaur V of the Vulcan rocket.

<span class="mw-page-title-main">Blue Origin</span> American aerospace company

Blue Origin Enterprises, L.P., commonly referred to as Blue Origin is an American aerospace manufacturer, government contractor, launch service provider, and space technologies company headquartered in Kent, Washington, United States. The company makes rocket engines for United Launch Alliance (ULA)'s Vulcan rocket and manufactures their own rockets, spacecraft, satellites, and heavy-lift launch vehicles. The company is the second provider of lunar lander services for NASA's Artemis program and was awarded a $3.4 billion contract. The four rocket engines the company has in production are the BE-3U, BE-3PM, BE-4 and the BE-7.

<span class="mw-page-title-main">Atlas V</span> Expendable launch system

Atlas V is an expendable launch system and the fifth major version in the Atlas launch vehicle family. It was designed by Lockheed Martin and has been operated by United Launch Alliance (ULA) since 2006. It is used for DoD, NASA, and commercial payloads. It is America's longest-serving active rocket. After 87 launches, in August 2021 ULA announced that Atlas V would be retired, and all 29 remaining launches had been sold. As of July 2024, 15 launches remain. Production ceased in 2024. Other future ULA launches will use the Vulcan Centaur rocket.

<span class="mw-page-title-main">Graphite-Epoxy Motor</span> American solid rocket booster

The Graphite-Epoxy Motor (GEM) is a family of solid rocket boosters developed in the late 1980s and used since 1990. GEM motors are manufactured with carbon-fibre-reinforced polymer casings and a fuel consisting of HTPB-bound ammonium perchlorate composite propellant. GEM is produced by Northrop Grumman Space Systems. GEM boosters are used on the Atlas V and were previously used on the Delta II, Delta III, and Delta IV launch vehicles. A new variant, the GEM 63XL, flew as part of the Vulcan Centaur launch vehicle on 8 January 2024.

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<span class="mw-page-title-main">Vandenberg Space Launch Complex 3</span> Launch site at Vandenberg Space Force Base in California

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<span class="mw-page-title-main">United Launch Alliance</span> Joint venture of Lockheed Martin and Boeing

United Launch Alliance, LLC (ULA) is an American launch service provider formed in December 2006 as a joint venture between Lockheed Martin Space and Boeing Defense, Space & Security. The company designs, assembles, sells and launches rockets, but the company subcontracts out the production of rocket engines and solid rocket boosters.

<span class="mw-page-title-main">Atlas III</span> American medium expendable launch vehicle

The Atlas III was an American orbital launch vehicle, used in the years between 2000 and 2005. It was developed from the highly successful Atlas II rocket and shared many components. It was the first member of the Atlas family since the Atlas A to feature a "normal" staging method, compared to the previous Atlas family members, which were equipped with two jettisonable outboard engines on the first (booster) stage. The Atlas III was developed further to create the Atlas V.

<span class="mw-page-title-main">Atlas (rocket family)</span> Family of American missiles and space launch vehicles

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<span class="mw-page-title-main">Delta IV Heavy</span> Variant of the Delta IV space launch vehicle

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<span class="mw-page-title-main">Astrobotic Technology</span> American space robotics company

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The Advanced Cryogenic Evolved Stage (ACES) was a proposed liquid oxygen/liquid hydrogen upper-stage for use on a number of different launch vehicles produced by Boeing, Lockheed Martin, United Launch Alliance (ULA). During the last five years of the program, ACES was proposed for eventual use on the Vulcan space launch vehicle designed by the U.S. company United Launch Alliance. The ACES concept had the objective to improve the on-orbit lifespan of current upper stages.

<span class="mw-page-title-main">BE-3</span> Liquid hydrogen/oxygen rocket engine

The BE-3 is a liquid hydrogen/liquid oxygen rocket engine developed by Blue Origin.

<span class="mw-page-title-main">BE-4</span> Large methalox fuelled staged-combustion rocket engine by Blue Origin

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<span class="mw-page-title-main">New Glenn</span> Launch vehicle developed by Blue Origin

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<span class="mw-page-title-main">Peregrine Mission One</span> Lunar lander built by Astrobotic Technology

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