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The Inertial Upper Stage (IUS), originally designated the Interim Upper Stage, was a two-stage, solid-fueled space launch system developed by Boeing for the United States Air Force beginning in 1976 for raising payloads from low Earth orbit to higher orbits or interplanetary trajectories following launch aboard a Titan 34D or Titan IV rocket, or from the payload bay of the Space Shuttle. Inertial Upper Stage neboli IUS je na tuhé pohonné látky, vyvinutý společností Boeing pro americké letectvo a NASA. Stupeň byl navržen k vynášení velkých nákladů z nákladového prostoru raketoplánu Space Shuttle, nebo mohl startovat s raketou Titan III jako její poslední stupeň. L'Inertial Upper Stage (IUS), è un razzo a due stadi a propellente solido sviluppato dalla US Air Force per il lancio di grandi carichi utili che avvengono sia da un (successivamente ) o dalla stiva dello Space Shuttle. L'étage Inertial Upper Stage, ou IUS (« Étage supérieur inertiel », initialement désigné « Interim Upper Stage »), est un étage supérieur de fusée développé par la société Boeing pour répondre aux besoins de lancement de satellites géostationnaires et de sondes spatiales par la navette spatiale américaine, en attendant la mise au point du remorqueur spatial « Space Tug ». «Inertial Upper Stage» — двухступенчатый твердотопливный разгонный блок для перемещения выводимых полезных грузов с опорной орбиты на целевую орбиту или межпланетные траектории. Использовался как последняя ступень в составе ракет-носителей Titan 34D, Titan IV или запускался в грузовом отсеке Спейс шаттла. Разработан корпорацией Boeing. O Inertial Upper Stage (IUS), originalmente designado de Interim Upper Stage, era um foguete de dois estágios de combustível sólido. O estágio superior foi desenvolvido pela Boeing para a Força Aérea dos Estados Unidos a partir de 1976 para lançar cargas na órbita terrestre baixa ou em órbitas ou trajetórias interplanetárias após o lançamento a bordo de um foguete Titan 34D ou Titan IV, ou a partir do compartimento de carga do ônibus espacial. 慣性上段ロケット(かんせいじょうだんロケット、英: Inertial Upper Stage: IUS, 元々は Interim Upper Stageとして知られていた)または慣性誘導上段ロケット(かんせいゆうどうじょうだんロケット)とは、二段構成の固体ロケットエンジンである。アメリカ空軍によって開発された。開発目的はタイタンIIIロケット、タイタン 34D、(後にタイタンIV)、またはスペースシャトルの貨物室から重くて大きなペイロードを打ち上げるためである。 Inertial Upper Stage (IUS) – dwusilnikowy górny człon rakietowy, wykorzystywany do wynoszenia satelitów na orbity geostacjonarne bądź trajektorie ucieczkowe. Wykorzystywany w rakietach i Titan IV oraz przy niektórych startach promów kosmicznych. Die IUS (Inertial Upper Stage, deutsch etwa: „Trägheitsnavigierte Oberstufe“, oder ursprünglich Interim Upper Stage, deutsch etwa: vorläufige Oberstufe) ist ein von Boeing hergestelltes, zweistufiges Modul, um Satelliten aus einer niedrigen Erdumlaufbahn in einen geostationären Orbit oder eine interplanetare Umlaufbahn zu bringen. Die IUS ist um alle drei Raumachsen stabilisiert und hat zwei Feststoffraketenmotoren, Orbus-21 und Orbus-6, für die beiden Impulsstöße einer Hohmannbahn. * Shuttle: 2268 kg * Titan-34D: 1817 kg * Titan-4A: 2364 kg * Titan-4B: 2860 kg Inertial Upper Stage (IUS) är en tvåstegs fastbränsleraket som utvecklats av USA:s flygvapen, för att användas tillsammans med eller med rymdfärjan. Första gången IUS användes var 1982 tillsammans med en Titanraket. IUS användes också i rymdsonden Galileos uppdrag 1989. Rymdsonden sköts upp med rymdfärjan Atlantis. Inertial Upper Stage (IUS), awalnya dinamakan Interim Upper Stage, adalah roket berbahan bakar padat tahap atas dua tahap yang dikembangkan oleh Boeing untuk Angkatan Udara Amerika Serikat. Dimulai pada tahun 1976 untuk menaikkan muatan dari orbit Bumi rendah ke orbit yang lebih tinggi atau lintasan antar berikut peluncuran kapal Titan 34D atau Titan IV roket, atau dari teluk payload dari Space Shuttle.
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Painting of Ulysses deploying from the Space Shuttle
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1982-10-30
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Inertial Upper Stage (IUS) är en tvåstegs fastbränsleraket som utvecklats av USA:s flygvapen, för att användas tillsammans med eller med rymdfärjan. Första gången IUS användes var 1982 tillsammans med en Titanraket. IUS användes också i rymdsonden Galileos uppdrag 1989. Rymdsonden sköts upp med rymdfärjan Atlantis. Inertial Upper Stage (IUS) – dwusilnikowy górny człon rakietowy, wykorzystywany do wynoszenia satelitów na orbity geostacjonarne bądź trajektorie ucieczkowe. Wykorzystywany w rakietach i Titan IV oraz przy niektórych startach promów kosmicznych. Die IUS (Inertial Upper Stage, deutsch etwa: „Trägheitsnavigierte Oberstufe“, oder ursprünglich Interim Upper Stage, deutsch etwa: vorläufige Oberstufe) ist ein von Boeing hergestelltes, zweistufiges Modul, um Satelliten aus einer niedrigen Erdumlaufbahn in einen geostationären Orbit oder eine interplanetare Umlaufbahn zu bringen. Die IUS ist um alle drei Raumachsen stabilisiert und hat zwei Feststoffraketenmotoren, Orbus-21 und Orbus-6, für die beiden Impulsstöße einer Hohmannbahn. Ursprünglich nur als Zwischenlösung bis zur Einführung der Centaur-G-Stufe auf dem Space Shuttle gedacht (daher der ursprüngliche Name), wurde die IUS nach der Einstellung des Shuttle-Centaur-Programms zur Standardoberstufe für schwere geostationäre Nutzlasten und Tiefraummissionen. Die IUS wurde sowohl auf Raketen vom Typ Titan-34D, Titan-4A-, Titan-4B als auch vom Space Shuttle eingesetzt. Die Nutzlastkapazitäten in den geostationären Orbit waren wie folgt: * Shuttle: 2268 kg * Titan-34D: 1817 kg * Titan-4A: 2364 kg * Titan-4B: 2860 kg Nutzlasten waren neben TDRSS-Kommunikationssatelliten und militärischen Satelliten die NASA-Missionen Magellan, Ulysses, Galileo und Chandra. Beim Start der Raumsonde Ulysses wurde die IUS mit einer zusätzlichen PAM-S-Oberstufe ausgestattet, um Ulysses auf eine besonders hohe Fluchtgeschwindigkeit zu bringen. O Inertial Upper Stage (IUS), originalmente designado de Interim Upper Stage, era um foguete de dois estágios de combustível sólido. O estágio superior foi desenvolvido pela Boeing para a Força Aérea dos Estados Unidos a partir de 1976 para lançar cargas na órbita terrestre baixa ou em órbitas ou trajetórias interplanetárias após o lançamento a bordo de um foguete Titan 34D ou Titan IV, ou a partir do compartimento de carga do ônibus espacial. L'étage Inertial Upper Stage, ou IUS (« Étage supérieur inertiel », initialement désigné « Interim Upper Stage »), est un étage supérieur de fusée développé par la société Boeing pour répondre aux besoins de lancement de satellites géostationnaires et de sondes spatiales par la navette spatiale américaine, en attendant la mise au point du remorqueur spatial « Space Tug ». Après l'abandon de ce dernier, puis l'arrêt de l'adaptation de l'étage à hydrogène liquide Centaur après l'accident de la navette Challenger, l'IUS devient incontournable pour le lancement de satellites depuis la navette. Sa conception lui permet de servir d'étage supérieur au lanceur militaire Titan. Il comprend deux étages, utilisant chacun un propulseur à propergol solide. Capable de placer un satellite de 2 à 3 tonnes sur une orbite géostationnaire, il est utilisé à 24 reprises de 1982 à 2004 pour lancer des satellites de télécommunications, des satellites militaires et des sondes spatiales, ainsi qu'un télescope spatial. L'arrêt des lancements de satellite depuis la navette spatiale, trop coûteux, puis le remplacement du lanceur Titan par les nouveaux lanceurs Atlas V et Delta IV, entraînent son retrait du service. Son dernier vol a lieu en février 2004. Inertial Upper Stage (IUS), awalnya dinamakan Interim Upper Stage, adalah roket berbahan bakar padat tahap atas dua tahap yang dikembangkan oleh Boeing untuk Angkatan Udara Amerika Serikat. Dimulai pada tahun 1976 untuk menaikkan muatan dari orbit Bumi rendah ke orbit yang lebih tinggi atau lintasan antar berikut peluncuran kapal Titan 34D atau Titan IV roket, atau dari teluk payload dari Space Shuttle. 慣性上段ロケット(かんせいじょうだんロケット、英: Inertial Upper Stage: IUS, 元々は Interim Upper Stageとして知られていた)または慣性誘導上段ロケット(かんせいゆうどうじょうだんロケット)とは、二段構成の固体ロケットエンジンである。アメリカ空軍によって開発された。開発目的はタイタンIIIロケット、タイタン 34D、(後にタイタンIV)、またはスペースシャトルの貨物室から重くて大きなペイロードを打ち上げるためである。 The Inertial Upper Stage (IUS), originally designated the Interim Upper Stage, was a two-stage, solid-fueled space launch system developed by Boeing for the United States Air Force beginning in 1976 for raising payloads from low Earth orbit to higher orbits or interplanetary trajectories following launch aboard a Titan 34D or Titan IV rocket, or from the payload bay of the Space Shuttle. L'Inertial Upper Stage (IUS), è un razzo a due stadi a propellente solido sviluppato dalla US Air Force per il lancio di grandi carichi utili che avvengono sia da un (successivamente ) o dalla stiva dello Space Shuttle. Inertial Upper Stage neboli IUS je na tuhé pohonné látky, vyvinutý společností Boeing pro americké letectvo a NASA. Stupeň byl navržen k vynášení velkých nákladů z nákladového prostoru raketoplánu Space Shuttle, nebo mohl startovat s raketou Titan III jako její poslední stupeň. «Inertial Upper Stage» — двухступенчатый твердотопливный разгонный блок для перемещения выводимых полезных грузов с опорной орбиты на целевую орбиту или межпланетные траектории. Использовался как последняя ступень в составе ракет-носителей Titan 34D, Titan IV или запускался в грузовом отсеке Спейс шаттла. Разработан корпорацией Boeing.
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