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#1
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From a CNN article
(http://www.cnn.com/2005/TECH/space/0...tle/index.html): To help find the malfunction, NASA has brought out of retirement an engineer who designed part of the sensor system back in the 1970s, said Wayne Hale, deputy shuttle program manager. This highlights how old the shuttle really is, and shows how hard it is to keep aging systems going. Jeff -- Remove icky phrase from email address to get a valid address. |
#2
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![]() "Jeff Findley" wrote in message ... From a CNN article (http://www.cnn.com/2005/TECH/space/0...tle/index.html): To help find the malfunction, NASA has brought out of retirement an engineer who designed part of the sensor system back in the 1970s, said Wayne Hale, deputy shuttle program manager. This highlights how old the shuttle really is, and shows how hard it is to keep aging systems going. A SpaceRef article (http://www.spaceref.com/news/viewsr.html?pid=17379) that has the following quote: Space Shuttle Program has not formally assessed the risk of aging and damaged wiring in accordance with NASA Procedural Requirements (NPR) 8000.4, "Risk Assessment Procedures," or developed a risk mitigation plan based on such an assessment. This does not bode well. Jeff -- Remove icky phrase from email address to get a valid address. |
#3
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Exactly what kinf of sensor is the ECO sensor?
I have seen some blcok diagrams of the total system but not a detailed electrical schematic diagram. Is there one posted anywhere on the web? "Jeff Findley" wrote in message ... "Jeff Findley" wrote in message ... From a CNN article (http://www.cnn.com/2005/TECH/space/0...tle/index.html): To help find the malfunction, NASA has brought out of retirement an engineer who designed part of the sensor system back in the 1970s, said Wayne Hale, deputy shuttle program manager. This highlights how old the shuttle really is, and shows how hard it is to keep aging systems going. A SpaceRef article (http://www.spaceref.com/news/viewsr.html?pid=17379) that has the following quote: Space Shuttle Program has not formally assessed the risk of aging and damaged wiring in accordance with NASA Procedural Requirements (NPR) 8000.4, "Risk Assessment Procedures," or developed a risk mitigation plan based on such an assessment. This does not bode well. Jeff -- Remove icky phrase from email address to get a valid address. |
#4
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![]() "Dave" wrote in message om... Exactly what kinf of sensor is the ECO sensor? I have seen some blcok diagrams of the total system but not a detailed electrical schematic diagram. Is there one posted anywhere on the web? I can't find an actual schematic (I'd love to see one). What I did find is NASA document title "Sensors and Electronics, LH2/LO2 Point Level, ECO". The sensor heads are described as "point sensor transducers". If I had to guess a bit, I'd say each end of the already mentioned platinum wire is connected to a pin in the sensor head. The wire loop is used as a thermometer. Run some current through it, measure the voltage, and pass that through the transducer. The result will be different when wet vs dry. |
#5
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"Jeff Findley" wrote:
From a CNN article (http://www.cnn.com/2005/TECH/space/0...tle/index.html): To help find the malfunction, NASA has brought out of retirement an engineer who designed part of the sensor system back in the 1970s, said Wayne Hale, deputy shuttle program manager. This highlights how old the shuttle really is, and shows how hard it is to keep aging systems going. Frankly, if we ever have routine spaceflight - I'd expect the same thing. Look at the ages of some of the aircraft still in revenue service. D. -- Touch-twice life. Eat. Drink. Laugh. -Resolved: To be more temperate in my postings. Oct 5th, 2004 JDL |
#6
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![]() "Derek Lyons" wrote in message ... "Jeff Findley" wrote: From a CNN article (http://www.cnn.com/2005/TECH/space/0...tle/index.html): To help find the malfunction, NASA has brought out of retirement an engineer who designed part of the sensor system back in the 1970s, said Wayne Hale, deputy shuttle program manager. This highlights how old the shuttle really is, and shows how hard it is to keep aging systems going. Frankly, if we ever have routine spaceflight - I'd expect the same thing. Look at the ages of some of the aircraft still in revenue service. D. Nothing else with wings is half as complex as a shuttle. I saw a DC-3 overhead yesterday. One of the reasons DC-3s are still in the air is that you can fix most of one with the tools you keep in the garage. |
#8
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![]() "Brian Gaff" wrote in message . uk... So are we saying that the wiring problem is in fact inside the orbiter? It would certainly explain why the other tank had a problem also, but not why the fault is affected by the tank being full or not, as that part of the equipment is in the tank, or would have to be to be affected. One assumes that there is at some point a connector that demates when the tank is jettisoned? Suspect no 1. I think it's a strong possibility, that and the electronics boxes in the orbiter that were likely made in the 70's as well. Even though they swapped them, who's to say that there isn't similar degradation in the two units due to heat, cold, corrosion, age, vibration, and etc.? Jeff -- Remove icky phrase from email address to get a valid address. |
#9
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Dave wrote:
Exactly what kinf of sensor is the ECO sensor? I have seen some blcok diagrams of the total system but not a detailed electrical schematic diagram. Is there one posted anywhere on the web? ---clip--- Harwood/CBS has a good general description and history of the system with photos at: http://www.spaceflightnow.com/shuttl...716ecographic/ Another poster referenced a document by title which is available at http://www.jsc.nasa.gov/news/columbi.../031042704.pdf which describes the sensors in detail, eg. "0.0005 INCH DIAMETER PLATINUM WIRE SENSING ELEMENTS MOUNTED ON A CERAMIC FRAME." The "FAILURE MODES EFFECTS ANALYSIS" on pg. 8 of the document is interesing. It describes a number of false "wet" or "dry" failure modes due to circuit and connector failures. JJ Robinson II Houston, TX |
#10
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Jeff Findley wrote:
I think it's a strong possibility, that and the electronics boxes in the orbiter that were likely made in the 70's as well. Even though they swapped them, who's to say that there isn't similar degradation in the two units due to heat, cold, corrosion, age, vibration, and etc.? 1- Why han't anyone commented that the flaky sensor exhibited strange readings on the 13th of the month ????? NASA could have written off that launch because it was the 13th and launched the next day , confident the sensors would work :-) :-) :-) 2- While the electronics may be of 1970s design, it doesn't mean that they were built in the 1970s. Many items in the shuttle were replaced with new units of the same design. There are many stories of NASA paying the big bucks to have small runs of old electronic parts built in order to maintain its spare parts inventory. 3- Since the ET burns up, it is a fair bet that any electronics in the ET are new. |
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