Amplitude Calibration System Prototype Development Plan v2.0 Prototype 1: Semi-Transparent Vane System The tests of the first prototype of a semi-transparent vane (STV) calibration system have been made at the IRAM 30m telescope, with encouraging results. Further tests with this system are required to confirm that the STV concept can work at the 3% level. The test that needs to be made is to check that the losses in the vane are due to absorption to within 3%. This test will require a measurement of the transmission of the vane on an astronomical source with very good weather conditions. Unfortunately, the 30m telescope is unavailable for further tests; the feasibility of some astronomical tests at the ATF with evaluation front ends is being investigated. Tests are needed at frequencies for which both ALMA and the ATF operate, with 1.3mm and 3mm most critical. Prototype 2: Wire Grid Amplitude Calibration System Design and construction of a test prototype for a more advanced device containing a polarization grid has been stalled. This second prototype will allow us to study the anticipated advantages of using a grid, which are anticipated to allow calibration accuracy of 1%. In fact, in the previous observing tests made with Prototype 1 at the IRAM 30m telescope, some preliminary measurements with the grids of the 30m receivers have been made. These tests were quite encourageing, and we are confident that tests could be made which would allow for a precision of about 1%. These tests will be pursued at (insert name of lab at Madrid) at a maximum frequency of 60 GHz. Tests are needed at frequencies for which ALMA operates, with 1.3mm and 3mm most critical. These tests might be pursued at the ATF. Prototype 3: Multi-Load Amplitude Calibration System This more advanced design would incorporate the concepts detailed in ALMA Memo 461. Three types of couplers will be tested and compared: semi-transparent vane; wire grid; dielectric film. An ALMA design will be developed, and testing will be performed at the ATF telescopes with ALMA prototype front ends, currently planned to be available for Q3 2005. Tests are needed at frequencies for which both ALMA and the ATF operate, with 1.3mm and 3mm most critical.