apollo service module diagram



Apollo Command and Service Module Documentation . Als Brennstoff wurde Aerozin 50 verwendet, eine Mischung aus 50 % Hydrazin und 50 % Unsymmetrischem Dimethylhydrazin, als Oxidator kam Distickstofftetroxid zum Einsatz, eine lagerfähige hypergole Treibstoffkombination. Ausgestellt als Teil der Saturn V im, Bereitgehalten als Rettungsraumschiff für, Die Steuerung befand sich auf der linken Seite, dem Platz des, Sektor 1 war ein 50°-Segment und anfangs unbenutzt. In this image, you may find the Apollo 11 Command And Service Module Diagram. In no way does anatomynote.com claim ownership or responsibility for such items, and you should seek legal consent for any use of such materials from its owner. Die sechs Sektoren waren wie folgt belegt (Zählung links oben beginnend und im Gegenuhrzeigersinn, vom CM aus gesehen): Alle Tanks bestanden aus Titanblech von 1,36 mm Stärke. The 360 degrees around the center section is divided among two 50-degree (Sectors 1 and 4), two 60-degree (Sectors 3 and 6), and two 70-degree (Sectors 2 and 5) compartments. Project Apollo Drawings and Technical Diagrams : ... Apollo Command and Service Modules and Launch Escape System from Apollo Program Summary Report (April 1975) Command Module Interior from Apollo Training Manual "Apollo Spacecraft & Systems Familiarization" (March 13, 1968) It is believed the switches welded shut, allowing the temperature within the tank to rise to over 1000 degrees F. The gauges measuring the temperature inside the tank were designed to measure only to 80 F, so the extreme heating was not noticed. This valve prevents any RCS propellants from flowing backwards into the helium tanks. Each RCS quad has both a primary and a secondary propellant tank. Für die Phase der Landung und Bergung stand darüber hinaus eine UKW-Verbindung mit einer ungerichteten Antenne zur Verfügung.

from Apollo Program Summary Report (April 1975) Command Module Interior. The automatic coils receive commands to fire from the RJ/EC and the direct coil is commanded by the RHC.
The engines use monomethylhydrazine (MMH) as fuel and inhibited nitrogen tetroxide oxidizer, each engine has about 100 lbf (441.5 N) thrust. Apollo war ein Raumschiff, das Mitte der 1960er im Rahmen des Apollo-Programms von North American Aviation entwickelt wurde. Apollo Command Module Interior A view of each side of the Command Module, the part of the spacecraft that re-entered Earth. This happens regardless of which package is currently displayed. Zur eigenständigen Navigation war das CM mit einem eigenen Computer, dem Apollo Guidance Computer, und zwei Bedienkonsolen ausgerüstet. CST-100 | This is done to ensure a steady output of force when the engine is fired and minimize transients. Thrusters 1 and 2 control roll and 3 and 4 control either pitch or yaw, depending on the quad. Unterteilt war es in eine Mittel- sowie weitere sechs Außensektionen. Außerdem befanden sich dort Antennen und Signalleuchten, welche die Bergung auf See erleichterten, sowie aufblasbare Ballons, die das System aufrichteten, sofern die Landekapsel nach der Wasserung mit der Spitze nach unten schwamm. The roll engines are offset from one another to accommodate the quad's plumbing. Your email address will not be published. All oxygen stores were lost within about 3 hours, along with loss of water, electrical power, and use of the propulsion system. You have successfully signed up for our newsletter. Im Vorderteil waren Stabilisierungsschirme (drogue chutes) sowie drei große Hauptfallschirme untergebracht.

verschrottet, vielleicht aber auch zerlegt im, Kommandokapsel ausgestellt im Saturn V Center am, Nicht fertiggestellt. The lower picture shows the Apollo 13 Service Module and the location of the oxygen tanks relative to the other systems. If you have any question please do not hesitate to contact us. Für die Druckgasförderung befanden sich zwei kugelförmige Heliumtanks im Mittelteil des Moduls. The force from the resulting reaction provides attitude control. Das SM enthielt die Systeme, welche für einen längeren Aufenthalt im Weltraum und zum Manövrieren benötigt wurden.

Each quad's thrusters are numbered 1 through 4. o.) Anatomy is the amazing science. Eine Zweimanncrew hätte zu Skylab fliegen und die Crew abholen können. Description. Die Lebenserhaltungssysteme kontrollierten die Kabinenatmosphäre und hielten die Temperatur bei 22 °C. From left to right this gauge displays: package temperature, helium pressure, secondary fuel pressure, and either helium temperature or fuel quantity. 655 Jefferson Drive, SW

Das CM bot jedem Astronauten etwa zwei Kubikmeter Raum. Das CM hatte eine Masse von 5900 kg bei einer Höhe von 3,23 m und einen Durchmesser von 3,91 m. Neben zahlreichen technischen Systemen enthielt es den Aufenthaltsbereich der Astronauten. Should the RCS quantity fall too low, the caution and warning system will alert you, just as it would for temperatures. Die Funkkommunikation fand im S-Band statt, insbesondere über die große, schwenkbare, kleeblattförmige Richtantenne am Heck des Servicemoduls. 2 showed anomalies and would not empty correctly, possibly due to the damaged fill line.


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from Apollo Training Manual "Apollo Spacecraft & Systems Familiarization" (March 13, 1968) 2 in the service module. Please Click Like Button to Support Our Facebook Page!

In order for the automatic coils to function the SM RCS logic circuit breakers 8.C on MDC-8 must be closed. 2 oxygen tank to explode. These are labeled PRIM PRPLNT for the primary isolation valves and SEC PRPLNT for the secondary valves. Please do not forget to share this page and follow our social media to help further develop our website. 1 tank and parts of the interior of the service module and blew off the bay no. Project Apollo NASA Spacecraft Drawings and Technical Diagrams. Bei den Flügen von, Sektor 2 umfasste 70° und wurde für den ersten, größeren Oxidatortank verwendet. Each RCS quad has its own individual fuel and plumbing systems. The no. These heaters can be given current via their SM RCS - SM RCS HEATERS circuit breakers on MDC-8 8.B.

This fourth indicator displays one of two values, which can be selected by the SM RCS IND switch 2.F. SpaceShipOne, National Museum of the United States Air Force, Primary Guidance, Navigation and Control System, https://de.wikipedia.org/w/index.php?title=Apollo_(Raumschiff)&oldid=196909984, „Creative Commons Attribution/Share Alike“, verschiedene Tests, u. a. akustische Vibrationen und Falltests, Kommandokapsel demontiert im Rahmen der Apollo-1-Untersuchung. Anatomy is the amazing science. Nur das CM mit den drei Astronauten an Bord war mit einem Hitzeschild ausgestattet und für einen Wiedereintrit… Visit us in Washington, DC and Chantilly, VA to explore hundreds of the world’s most significant objects in aviation and space history. Der Sextant war über Winkelencoder direkt mit dem Computer verbunden, was von der Bauform gewöhnlicher Sextanten abwich. Es war bereits früher in einem Raumschiff eingesetzt, vor dem Start des früheren Raumschiffs jedoch wieder entfernt und trotz eines Defekts bei Apollo 13 verwendet worden. The sketches above are taken from the NASA book "Apollo Expeditions to the Moon", NASA SP-350. for more anatomy content please follow us and visit our website: www.anatomynote.com. Mercury |

Chantilly, VA 20151 A fuel injector valve consists of two separate coils, an automatic and direct coil. When an RCS engine fires, the fuel and oxidizer cross in the premix chamber first before entering the combustion chamber. The lunar module represents one of humanity’s greatest achievements: landing people on another heavenly body. Der innere Zylinder enthielt zwei kugelförmige Tanks mit Helium unter hohem Druck.

Your email address will not be published. It houses the electrical power subsystem, reaction control engines, part of the environmental control subsystem, and the service propulsion subsystem including the main propulsion engine for insertion into orbit around the moon, for return from the moon, and for course corrections. Das gesamte Triebwerk und die Triebwerksdüse waren 3,90 m lang und wogen zusammen 293 kg. Apollo Operations Handbook, Block II Spacecraft, Volume 1, Spacecraft Description, SM2A-03-Block II-(1), SID 66-1508, 15 October 1969, ( 8.4 Mb PDF).Scan and PDF formatting by Bill Wood. The propellant flow from the tanks to the thrust chambers is controlled by electric engine injector solenoid valves.

Die rückwärtigen Schränke wären gegen zwei weitere Liegen ausgetauscht und das Lebenserhaltungssystem entsprechend ergänzt worden. If you think this picture helpful, please don't forget to rate us below the picture!

If the square talkback indicator for a particular solenoid is barber-pole (meaning it displays white and black diagonals) the helium tank is blocked from the rest of the quad. Our Steven F. Udvar-Hazy Center in Virginia has reopened. What did that historic mission mean to you? Apollo Command and Service Modules and Launch Escape System Apollo Program Summary Report (April 1975) Command Module Interior from Apollo Training Manual"Apollo Spacecraft & Systems Familiarization"(March 13, 1968) We hope you can get the exact information you are looking for. for more anatomy content please follow us and visit our website: www.anatomynote.com. This diagram shows the configuration for the modules on Apollos 15, 16, 17--the only missions to carry a Lunar Roving Vehicle. The controls for these valves are located below the helium isolation valves on MDC-2 2.B and work in exactly the same manner. It can help you understand our world more detailed and specific. Eine Zündung im eigentlichen Sinn mittels Funken erfolgte nicht, die beiden Flüssigkeiten zünden bei Kontakt miteinander. Sorry, there was a problem. The injectors are all magnetically shut and must receive commands from either the RJ/EC or the RHC to open and fire. Service Module (SM-014) flog mit, evtl. Bei deren Rückkehr aus dem Weltraum diente es als Landekapsel. We are pleased to provide you with the picture named Apollo 11 Command And Service Module Diagram. The Service Module RCS contains 16 reaction control jets grouped into clusters of four, or quads. We hope you will use this picture in the study and helping your research.

The Service Module was typically detached and burned up on re-entry. Es bestand aus zwei Komponenten: dem Kommandomodul (CM) und dem Servicemodul (SM). One of our purpose to collect these pictures is we hope these pictures will not be lost when the relevant web page is deleted.

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from Apollo Program Summary Report (April 1975) Command Module Interior. The automatic coils receive commands to fire from the RJ/EC and the direct coil is commanded by the RHC.
The engines use monomethylhydrazine (MMH) as fuel and inhibited nitrogen tetroxide oxidizer, each engine has about 100 lbf (441.5 N) thrust. Apollo war ein Raumschiff, das Mitte der 1960er im Rahmen des Apollo-Programms von North American Aviation entwickelt wurde. Apollo Command Module Interior A view of each side of the Command Module, the part of the spacecraft that re-entered Earth. This happens regardless of which package is currently displayed. Zur eigenständigen Navigation war das CM mit einem eigenen Computer, dem Apollo Guidance Computer, und zwei Bedienkonsolen ausgerüstet. CST-100 | This is done to ensure a steady output of force when the engine is fired and minimize transients. Thrusters 1 and 2 control roll and 3 and 4 control either pitch or yaw, depending on the quad. Unterteilt war es in eine Mittel- sowie weitere sechs Außensektionen. Außerdem befanden sich dort Antennen und Signalleuchten, welche die Bergung auf See erleichterten, sowie aufblasbare Ballons, die das System aufrichteten, sofern die Landekapsel nach der Wasserung mit der Spitze nach unten schwamm. The roll engines are offset from one another to accommodate the quad's plumbing. Your email address will not be published. All oxygen stores were lost within about 3 hours, along with loss of water, electrical power, and use of the propulsion system. You have successfully signed up for our newsletter. Im Vorderteil waren Stabilisierungsschirme (drogue chutes) sowie drei große Hauptfallschirme untergebracht.

verschrottet, vielleicht aber auch zerlegt im, Kommandokapsel ausgestellt im Saturn V Center am, Nicht fertiggestellt. The lower picture shows the Apollo 13 Service Module and the location of the oxygen tanks relative to the other systems. If you have any question please do not hesitate to contact us. Für die Druckgasförderung befanden sich zwei kugelförmige Heliumtanks im Mittelteil des Moduls. The force from the resulting reaction provides attitude control. Das SM enthielt die Systeme, welche für einen längeren Aufenthalt im Weltraum und zum Manövrieren benötigt wurden.

Each quad's thrusters are numbered 1 through 4. o.) Anatomy is the amazing science. Eine Zweimanncrew hätte zu Skylab fliegen und die Crew abholen können. Description. Die Lebenserhaltungssysteme kontrollierten die Kabinenatmosphäre und hielten die Temperatur bei 22 °C. From left to right this gauge displays: package temperature, helium pressure, secondary fuel pressure, and either helium temperature or fuel quantity. 655 Jefferson Drive, SW

Das CM bot jedem Astronauten etwa zwei Kubikmeter Raum. Das CM hatte eine Masse von 5900 kg bei einer Höhe von 3,23 m und einen Durchmesser von 3,91 m. Neben zahlreichen technischen Systemen enthielt es den Aufenthaltsbereich der Astronauten. Should the RCS quantity fall too low, the caution and warning system will alert you, just as it would for temperatures. Die Funkkommunikation fand im S-Band statt, insbesondere über die große, schwenkbare, kleeblattförmige Richtantenne am Heck des Servicemoduls. 2 showed anomalies and would not empty correctly, possibly due to the damaged fill line.


We think this is the most useful anatomy picture that you need.

from Apollo Training Manual "Apollo Spacecraft & Systems Familiarization" (March 13, 1968) 2 in the service module. Please Click Like Button to Support Our Facebook Page!

In order for the automatic coils to function the SM RCS logic circuit breakers 8.C on MDC-8 must be closed. 2 oxygen tank to explode. These are labeled PRIM PRPLNT for the primary isolation valves and SEC PRPLNT for the secondary valves. Please do not forget to share this page and follow our social media to help further develop our website. 1 tank and parts of the interior of the service module and blew off the bay no. Project Apollo NASA Spacecraft Drawings and Technical Diagrams. Bei den Flügen von, Sektor 2 umfasste 70° und wurde für den ersten, größeren Oxidatortank verwendet. Each RCS quad has its own individual fuel and plumbing systems. The no. These heaters can be given current via their SM RCS - SM RCS HEATERS circuit breakers on MDC-8 8.B.

This fourth indicator displays one of two values, which can be selected by the SM RCS IND switch 2.F. SpaceShipOne, National Museum of the United States Air Force, Primary Guidance, Navigation and Control System, https://de.wikipedia.org/w/index.php?title=Apollo_(Raumschiff)&oldid=196909984, „Creative Commons Attribution/Share Alike“, verschiedene Tests, u. a. akustische Vibrationen und Falltests, Kommandokapsel demontiert im Rahmen der Apollo-1-Untersuchung. Anatomy is the amazing science. Nur das CM mit den drei Astronauten an Bord war mit einem Hitzeschild ausgestattet und für einen Wiedereintrit… Visit us in Washington, DC and Chantilly, VA to explore hundreds of the world’s most significant objects in aviation and space history. Der Sextant war über Winkelencoder direkt mit dem Computer verbunden, was von der Bauform gewöhnlicher Sextanten abwich. Es war bereits früher in einem Raumschiff eingesetzt, vor dem Start des früheren Raumschiffs jedoch wieder entfernt und trotz eines Defekts bei Apollo 13 verwendet worden. The sketches above are taken from the NASA book "Apollo Expeditions to the Moon", NASA SP-350. for more anatomy content please follow us and visit our website: www.anatomynote.com. Mercury |

Chantilly, VA 20151 A fuel injector valve consists of two separate coils, an automatic and direct coil. When an RCS engine fires, the fuel and oxidizer cross in the premix chamber first before entering the combustion chamber. The lunar module represents one of humanity’s greatest achievements: landing people on another heavenly body. Der innere Zylinder enthielt zwei kugelförmige Tanks mit Helium unter hohem Druck.

Your email address will not be published. It houses the electrical power subsystem, reaction control engines, part of the environmental control subsystem, and the service propulsion subsystem including the main propulsion engine for insertion into orbit around the moon, for return from the moon, and for course corrections. Das gesamte Triebwerk und die Triebwerksdüse waren 3,90 m lang und wogen zusammen 293 kg. Apollo Operations Handbook, Block II Spacecraft, Volume 1, Spacecraft Description, SM2A-03-Block II-(1), SID 66-1508, 15 October 1969, ( 8.4 Mb PDF).Scan and PDF formatting by Bill Wood. The propellant flow from the tanks to the thrust chambers is controlled by electric engine injector solenoid valves.

Die rückwärtigen Schränke wären gegen zwei weitere Liegen ausgetauscht und das Lebenserhaltungssystem entsprechend ergänzt worden. If you think this picture helpful, please don't forget to rate us below the picture!

If the square talkback indicator for a particular solenoid is barber-pole (meaning it displays white and black diagonals) the helium tank is blocked from the rest of the quad. Our Steven F. Udvar-Hazy Center in Virginia has reopened. What did that historic mission mean to you? Apollo Command and Service Modules and Launch Escape System Apollo Program Summary Report (April 1975) Command Module Interior from Apollo Training Manual"Apollo Spacecraft & Systems Familiarization"(March 13, 1968) We hope you can get the exact information you are looking for. for more anatomy content please follow us and visit our website: www.anatomynote.com. This diagram shows the configuration for the modules on Apollos 15, 16, 17--the only missions to carry a Lunar Roving Vehicle. The controls for these valves are located below the helium isolation valves on MDC-2 2.B and work in exactly the same manner. It can help you understand our world more detailed and specific. Eine Zündung im eigentlichen Sinn mittels Funken erfolgte nicht, die beiden Flüssigkeiten zünden bei Kontakt miteinander. Sorry, there was a problem. The injectors are all magnetically shut and must receive commands from either the RJ/EC or the RHC to open and fire. Service Module (SM-014) flog mit, evtl. Bei deren Rückkehr aus dem Weltraum diente es als Landekapsel. We are pleased to provide you with the picture named Apollo 11 Command And Service Module Diagram. The Service Module RCS contains 16 reaction control jets grouped into clusters of four, or quads. We hope you will use this picture in the study and helping your research.

The Service Module was typically detached and burned up on re-entry. Es bestand aus zwei Komponenten: dem Kommandomodul (CM) und dem Servicemodul (SM). One of our purpose to collect these pictures is we hope these pictures will not be lost when the relevant web page is deleted.
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