______________________________________________________________________________ | File Name : MRATLDYN.ASC | Online Date : 10/28/95 | | Contributed by : Joel McClain | Dir Category : ENERGY | | From : KeelyNet BBS | DataLine : (214) 324-3501 | | KeelyNet * PO BOX 870716 * Mesquite, Texas * USA * 75187 | | A FREE Alternative Sciences BBS sponsored by Vanguard Sciences | | InterNet email keelynet@ix.netcom.com (Jerry Decker) | | Files also available at Bill Beaty's http://www.eskimo.com/~billb | |----------------------------------------------------------------------------| The following document is taken from .PCX images uploaded to KeelyNet by Joel which show verification of the MRA as an overunity device in a test conducted by Teledyne Ryan Aeronautical. This is the first and only MRA confirmation that has been uploaded to KeelyNet. The files take four forms : MRATLDYN.ASC - contains ASCII text of page 1 and page 2 of the .PCX images MRATLDN1.GIF - page 1 with the Teledyne header MRATLDN2.GIF - page 2 with the Teledyne header MRATLDN3.GIF - circuit layout and test setups MRATLDN.ZIP - all of the above files are bundled into one master file ------------------------------------------------------------------------------ Teledyne Ryan Aeronautical 2701 N. Harbor Drive PO BOX 84311 San Diego, CA 92186-5311 (619) 291-7311 FAX (619) 250-5400 Letter of Cerfification 26 September 1995 329/95-07/REE To : Karel Taylor, OPS P.O. Box 461793 Escondido, CA 92046 (Taylor Construction 404-587-3454) From : Teledyne Ryan Aeronautical Engineering Environmental Laboratory 2701 Harbor Drive P.O. Box 85311 San Diego, CA 82186-5311 Subject : Measurement Verification References : (a) Telecon, 18 September 1995, K. Taylor and R. Chalmers of TRA (b) TAR Quote ENV 4248 Introduction One (1) MRA S/N 95-3 was setup for demonstration and measurement verification on 25 September 1995. The demonstration and measurements were performed at the Teledyne Ryan Aeronautical (TRA) Engineering Environmental Laboratory located in San Diego, California. The demonstration was conducted by Robert Taylor and the measurement verification was performed by Ed Everett of Teledyne Ryan Aeronautical. The MRA demonstration and measurement verification was conducted according to customer direction. No written plan/guideline was provided. A chronological record of the event was maintained and is identified as TR 3715. The test log was used as the basis of this report and a copy of this log is presented as Attachment A. A copy of the equipment list is also included as Attachment B. A short discussion of the measurements made is provided below. Discussion The customer setup the MRA as shown in Figure 1. Using his own signal generator, power amplifier and measurement meter, the customer demonstrated the MRA to his visitors. After his demonstration and discussion, the MRA circuit was connected to a TRA RF signal generator, (Rohde & Schwarz model 845.4002.44), as shown in Figure 2. The following conditions/assumptions apply: a) The MRA was treated as a Black Box with an input (A & B) and an output (D & E). b) The input circuit was considered a series circuit i.e. the current flow R1 & R2 represents the total input current. c) No examination of the MRA was made other than a cursory visual inspection of the exterior. Using a TRA oscilloscope, (Tektronix model 2205), the following measurements were made: 1) The signal generator was set to 91.412 Khz per the customer, and the output was turned up to the maximum level. 2) The input to the MRA (points A to B) was measured and found to be 0.085 Volts peak (Vpk), or 0.060 Volts RMS, (Vrms). 3) The voltage across R1 & R2 (B to C) was measured next and found to be 0.125 Vpk (0.088 Vrms). 4) The input current was then calculated per the customer as the voltage (rms) across R1 & R2 divided by the resistance of R1 + R2. This yields 0.3 uAmps. 5) The output voltage across R3 (D & E) was measured and found to be 0.015 Vpk (0.0106 Vrms). 6) The output current through R3 was calculated per the customer as the voltage (rms) across R3 divided by the resistance of R3. This yields 10.6 uAmps. 7) The customer defines the MRA gain as the output voltage (rms) D to E times the output current through R3 divided by the input voltage (rms) A to B times the input current through R1 & R2. This yields (0.0106 X 10.6 X 10 to the minus 6th) = 6.2 8) The customer removed the input to the MRA at points A & B. The output across R3 was measured again and was found to be approximately 1 to 2 millivolts of noise. The frequency of all voltages measured was 91.412 Khz except for step 8 which was random noise. ------------------------------------------------------------------------------