Английская Википедия:Booster separation motor

Материал из Онлайн справочника
Перейти к навигацииПерейти к поиску

Шаблон:More references

Файл:STS-117 SRB Separation.webm
Booster separation motors fire

The booster separation motors or BSMs on the Space Shuttle were relatively small rocket motors that separated the reusable solid rocket boosters (SRB) from the orbiter after SRB burnout. Eight booster separation motors were attached to each of the shuttle's two reusable solid rocket boosters, four on the forward frustum and four on the aft skirt.[1][2][3]

About two minutes into a Space Shuttle flight, all 16 of these motors were fired simultaneously for 1.2 seconds, providing the precise thrust required to safely separate the spent boosters from the Space Shuttle's external tank and orbiter, while traveling more than Шаблон:Convert and an altitude of approximately Шаблон:Convert.

The booster separation motors were produced by ATK Launch Systems Group, part of Alliant Techsystems (ATK) Inc., at their facility in Brigham City, Utah. The Booster separation motors each weighed Шаблон:Convert when loaded with propellant, and Шаблон:Convert when empty. They were Шаблон:Convert long and Шаблон:Convert in diameter.[4]

Northrop Grumman is now manufacturing the booster separation motors for the Space Launch System Boosters, part of the NASA Space Launch System (SLS) for the Artemis program.[5]

For Ariane 5 and Ariane 6, a Norwegian-Finnish company Nammo manufactures similar but different booster separation motors.[6]

References

Шаблон:ReflistШаблон:Space Shuttle Шаблон:Artemis program