(Q22001987)

English

AJ-60A

solid rocket booster by Aerojet Rocketdyne

Atlas V Solid Rocket Motor

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Atlas V SRB without Nose cone.jpg
2,000 × 3,008; 511 KB

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mass

46,697 kilogram

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reference URL

https://web.archive.org/web/20110930101856/http://www.ulalaunch.com/site/docs/product_cards/guides/AtlasVUsersGuide2010.pdf

country of origin

United States of America

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1999

2003

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reference URL

https://web.archive.org/web/20170314072244/http://www.rocket.com/atlas-v-solid-rocket-motor

17 July 2003

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2020

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17 July 2003

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height

16.9926 metre

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reference URL

https://web.archive.org/web/20170314072244/http://www.rocket.com/atlas-v-solid-rocket-motor

diameter

1.5748 metre

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reference URL

https://web.archive.org/web/20170314072244/http://www.rocket.com/atlas-v-solid-rocket-motor

source of energy

solid rocket propellant

has part(s)

hydroxyl-terminated polybutadiene

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2003

2020

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maximum thrust

1,688.4 kilonewton

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reference URL

https://web.archive.org/web/20110930101856/http://www.ulalaunch.com/site/docs/product_cards/guides/AtlasVUsersGuide2010.pdf

Commons category

AJ60A (rocket engine)

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Identifiers

Google Knowledge Graph ID

/g/11ckxxj2bb

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Sitelinks

Wikipedia(6 entries)

cawiki AJ-60A
enwiki AJ-60A
frwiki AJ-60A
plwiki AJ-60A
ptwiki AJ-60A
ukwiki AJ-60A

(Q22001987)

AJ-60A

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Wikipedia(6 entries)

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