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CRYOGENICS AND ITS SPACE APPLICATIONS full report


Posted by: project report tiger
Created at: Monday 15th of February 2010 08:04:22 AM
Last Edited Or Replied at :Sunday 21st of March 2010 03:24:18 AM
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a sample of gas forms a straight line. (This assumes that you keep the pressure constant.) The lower the temperature, the lower the volume. If you extend this line to low enough temperatures, it will eventually hit zero volume. Scientists noticed that, for all gasses, the temperature at which the graph said they would reach zero volume was about -273 Celsius (about -460 Fahrenheit).
This temperature became known as absolute zero, and is today the zero for the Kelvin and Rankine temperature scales. Nowadays, we know that gasses do not shrink to zero volume when cooled to absolute zero, becau..................[:=> Show Contents <=:]



composite materials for aerospace applications ppt


Posted by: chinna518
Created at: Monday 01st of March 2010 10:41:47 AM
Last Edited Or Replied at :Sunday 28th of March 2010 04:09:44 PM
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send me this topic..................[:=> Show Contents <=:]



composite materials for aerospace applications ppt


Posted by: sri.2988
Created at: Thursday 25th of February 2010 06:12:22 AM
Last Edited Or Replied at :Wednesday 04th of May 2011 05:17:45 AM
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CRYOGENICS AND ITS SPACE APPLICATIONS full report


Posted by: project report tiger
Created at: Monday 15th of February 2010 08:04:22 AM
Last Edited Or Replied at :Sunday 21st of March 2010 03:24:18 AM
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S, there are four stages of cooling.
The primary source of cooling is a 130 liter solid neon dewar. The life of the neon is extended by the use of a mechanical cooler which cools the outer radiation shield of the dewar. The solid neon maintains a temperature of 17 K, and surrounds a 32 liter tank filled with liquid helium. The liquid helium is vented to space, and maintains a temperature of K. The final stage of cooling is accomplished via the use of an adiabatic demagnetization refrigerator (ADR). This allows operation down to 50 mK; for the XRS, the nominal operating temperature will be 6..................[:=> Show Contents <=:]



Microphotonics for Space Application full report


Posted by: project reporter
Created at: Monday 01st of February 2010 01:25:34 AM
Last Edited Or Replied at :Friday 04th of June 2010 04:06:00 AM
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aveguide/MEMS optical accelerometers
5. Si Sun sensor or VOn bolometric IR Earth sensor quadrant arrays
6. waveguide optical gyroscope (optional development)
The end result is an orders of magnitude saving in the system mass and volume. This facilitates greater device redundancy to reduce the possibility of a systems failure. Moreover, redundancy can also be used to improve the net performance and accuracy of the navigation measurement systems.
Fig. 3-1: Preliminary concept of two-axis spacecraft navigation micro-PIC.
The PBG/MEMS structure devised by MPB for the 2x2 switch function can ..................[:=> Show Contents <=:]



METALLURGICAL CHANGES IN STEELS DUE TO CRYOGENIC PROCESSING ITS APPLICATIONS


Posted by: computer science technology
Created at: Sunday 24th of January 2010 11:20:47 AM
Last Edited Or Replied at :Sunday 24th of January 2010 11:20:47 AM
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resistant surface, higher yield and ultimate strength. This alloy will display structural, thermal and metallurgical stability not found in the untreated condition, as well as significant abrasive wear improvement. The contact and fretting fatigue will be reduced due to the tightening of the surface microstructure. In addition, the corrosion resistance to hot reactive gases and moisture in the combustion chamber will be improved.
COMPACT DISCS:
Compact disks respond to cryogenic treatment. Understanding this is hard to fathom, but it is quite true. The effect is a permanent increase in the..................[:=> Show Contents <=:]



Composites materials for aerospace applications full report


Posted by: computer science technology
Created at: Sunday 24th of January 2010 07:49:09 AM
Last Edited Or Replied at :Sunday 24th of January 2010 07:49:09 AM
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y prepreg For Lightning Strike protection Wing-skin, others
E-glass fabric in epoxy resins
High temp curing
RT / moderate temp curing Fighters fairings, fin-radome, drop-tanks, Small transport air craft structural components : Fuselage, wing, others

Some other aerospace applications are illustrated above:
Fig. A : Two seater transport aircraft
Fig. B : Space launch vehicles (Space Shuttles)
Fig. C : Satellites
Fig. D : Advanced helicopters (Military & Civilian)
6. Advances in materials for composites
6.1 Reinforcements
The carbon fibre technology continues to improve harnes..................[:=> Show Contents <=:]



CRYOGENICS


Posted by: seminar projects crazy
Created at: Friday 30th of January 2009 12:58:28 PM
Last Edited Or Replied at :Saturday 08th of December 2012 03:28:21 AM
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ce, physics research etc. Rocket propulsion is imparting force to a flying vehicle such as missile or spacecraft. Different types of rockets and their parts are explained. Cryogenics has future applications in many fields like superconductivity and propulsion fields. Cryogenics is being applied to variety of research areas; a few of which are: food processing and refrigeration, space craft life supporting system, space simulation, microbiology, medicine, surgery, electronics, data processing and metal working. Rocket propulsion is the process of imparting a force to flying vehicle such as a mi..................[:=> Show Contents <=:]



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