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SPACE LAUNCH SYSTEM

The Space Launch System is an advanced heavy-lift launch vehicle designed for science and human exploration beyond low Earth orbit. While NASA's commercial partners will provide the supply line to the International Space Station, the SLS will able to provide backup transportation to the ISS if the need arises.

The SLS will be the most powerful rocket in history with the initial stage of development able to provide 8.4 million pounds of thrust at liftoff, weigh in at 5.5 million pounds, and carry 154,000 pounds (nearly 70 metric tons) of payload. Later versions will be even more powerful with payload capacities of 105 and 130 metric tons. With 8.4 million pounds of thrust, the SLS will exceed the thrust of the Saturn V by 10 percent.

The first SLS mission, Exploration Mission 1, is tentatively scheduled for 2017 and will launch an uncrewed Orion spacecraft to the moon and back to demonstrate integrated system performance. The second SLS mission, Exploration Mission 2, is targeted for 2021 and will launch an Orion with a crew of up to four to the moon and back. These would be the only flights of the Block 1 configuration, then being replaced by Block 1A.

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A comparison of the SLS configurations, with the initial Block 1 configuration on the left (NASA)


Block 1 Configuration
  • Block 1 uses two 5-segment expendable SRBv boosters.
  • The SRBv solid rocket fuel is polybutadiene acrylonitride (PBAN).
  • Core stage will contain four RS-25D engines
  • Core stage will be common across subsequent blocks.
  • Booster TVC uses STS SRB heritage hardware.
  • Block 1 is capable of carrying an Orion-MPCV, Orion-MPVC + Interim Cryogenic Propulsion Stage (ICPS), or cargo payload.
  • Cargo payloads will be responsible for orbit stabilization.
Quick specs
  • Weight: 5.5 million pounds  - Equivalent to 7.5 fully loaded 747 jets
  • Height: 321 feet - Taller than the Statue of Liberty
  • Payload: 70 metric tons (154,000 pounds) to orbit
  • Thrust: 8.4 million pounds
First flight projected for 2017, first manned flight 2021
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Block 1A Configuration
  • Block 1A encompasses replacement of the SRB with a new expendable advanced booster (SRB or LRB).
    - LRB uses Refined Petroleum (RP-1) propellant.
  • Advanced booster attaches at the same points as the SRBv.
  • Core stage incorporates the RS-25D or RS-25E engines.
    - Four engines on the core stage.
  • Block 1A uses a LH2/LOX stage that may have one or more AUSEs.
  • Block 1A is the same height ass the Block 1 configuration.
First flight projected for 2022, first manned flight 2025
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Block 2 Configuration
  • This upgrade add an upper stage that derives from the core stage.
  • One to three J-2X engines are used on the upper stage.
  • The upper stage uses the same propellant as the core stage.
Quick specs
  • Weight: 6.5 million pounds - Equivalent to 8.8 fully loaded 747 jets
  • Height: 384 feet - Tall as a 38 story building
  • Cargo volume: Could carry 9 school buses
  • Payload: 130 metric tons (286,000 pounds) to orbit
  • Thrust: 9.2 million pounds (20% greater than Saturn V)
First flight projected for 2032
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(Courtesy NASA)


rs-25.jpg  The Rocketdyne RS-25D rocket engine served as the Space Shuttle Main Engine (SSME) from July 2001 until the retirement of the shuttle fleet in 2011. The RS-25E is based on a 2005 proposal for a simplified SSME.

srb.jpg  SRBv (Solid Rocket Booster, 5 segment) is based on the same technology that the STS (space shuttle) used for its solid rocket boosters. ATK of Brigam City, Utah is the prime contractor and has begun processing the first hardware components for the initial qualification test planned for 2013.

J-2x.jpg  The J-2X engine is being developed by Pratt & Whitney Rocketdyne. The first engine being tested at the Stennis Space Center in 2011 achieved a 500 second, full flight duration burn during its eighth test.

The Interim Cryogenic Propulsion Stage (ICPS) is considered part of the payload and not the SLS itself. It will be present on both Block 1 flights and could appear in Block 1A as well. The ICPS can perform up to three burns, thus making lunar or other deep space destinations possible. ICPS specifications closely align with the existing Delta 4 Heavy upper stage. Solicitations for an ICPS were issued in May 2012.

 


Page last modified: 16 August 2015 17:48:57.