(Q109770367)

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Space Launch System Solid Rocket Booster

solid propellant rocket for NASA's Space Launch Ststem

5-segment Solid Rocket Booster
SLSSRB
5-segment SRB
five-segment Solid Rocket Booster
five-segment SRB

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SLS FSB1 test booster.jpg
1,200 × 681; 437 KB

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The second and final qualification motor (QM-2) test for the SLS Solid Rocket Booster on June 28, 2016, at Promontory, Utah. (English)

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726,000 kilogram

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https://www.nasa.gov/wp-content/uploads/2022/03/sls-reference-guide-2022-v2-508-0.pdf

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9

99,300 kilogram

criterion used

dry weight

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reference URL

https://www.nasa.gov/wp-content/uploads/2022/03/sls-reference-guide-2022-v2-508-0.pdf

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9

based on

Space Shuttle Solid Rocket Booster

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country of origin

United States of America

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manufacturer

Northrop Grumman Innovation Systems

end time

2020

start time

unknown value

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Northrop Grumman Space Systems

start time

2020

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height

54 metre

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reference URL

https://www.nasa.gov/wp-content/uploads/2022/03/sls-reference-guide-2022-v2-508-0.pdf

page(s)

9

diameter

3.7 metre

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reference URL

https://www.nasa.gov/wp-content/uploads/2022/03/sls-reference-guide-2022-v2-508-0.pdf

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9

source of energy

polybutadiene acrylonitrile

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reference URL

https://www.nasa.gov/wp-content/uploads/2022/03/sls-reference-guide-2022-v2-508-0.pdf

9

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Space Launch System Solid Rocket Boosters

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commonswiki Category:Space Launch System Solid Rocket Boosters