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[lNCti-POUNDl MIL-HDBK-244A 6 APRIL 1990 SUPERSEDING MIL-HDBK-244 1 AUGUST 1975 MILITARY HANDBOOK .. .. . . GUIDE TO AIRCRAFT/STORES COMPATIBILITY AMSC N/A FSC 15GP DISTRIBUTION STATEMENT A. Approvedfor public release; distribution is unlimited. Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:53Z Check the source to verify that this is the current version before use. MIL-HDBK-244A FOREWARD 1. This military handbook is approved for use of the Department of Defense. by all Departments and Agencies 2. Beneficial comments (recommendations,additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Naval Air Engineering Center, Systems Engineering and Standardization Department (Code 53), Lakehurst, NJ 08733-5100, by using the

e documents are available online at https://quicksearch.dla.mil). DEPARTMENT OF DEFENSE HANDBOOKS MIL-HDBK-235-1 Military Operational Electromagnetic Environment Profiles MIL-HDBK-240-2 Electromagnetic Environmental Effects to Ordnance Guide Part 2 Hazards of Electromagnetic Radiation to Ordnance Testing Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:47Z Check the source to verify that this is the current version before use. MIL-HDBK-516D 11 MIL-HDBK-240-3 Electromagnetic Environmental Effects to Ordnance Guide Part 3 Electrostatic Discharge to Ordnance MIL-HDBK-240-4 Electromagnetic Environmental Effects to Ordnance Guide Part 4 External Radio Frequency Electromagnetic Environments MIL-HDBK-244 Guide to Aircraft/Stores Compatibility MIL-HDBK-310 Global Climatic Data for Devel

) MIL-STD-1512 Electroexplosive Subsystems, Electrically Initiated, Design Requirements and Test Methods MIL-STD-1670 Environmental Criteria and Guidelines for Air-Launched Weapons MIL-STD-1760 Interface Standard for Aircraft/Store Electrical Interconnection System MIL-STD-1795 Lightning Protection of Aerospace Vehicles and Hardware MIL-STD-1818 Electromagnetic Effects Requirements for Systems MIL-STD-2105 Hazard Assessment Tests for Non-Nuclear Munitions MIL-STD-2167 Defense System Software Development (Canceled) MIL-STD-38784 Standard Practice for Manuals, Technical: General Style and Format Requirements HANDBOOKS MIL-HDBK-235-1 Electromagnetic (Radiated) Environment Considerations for Design and Procurement of Electrical and Electronic Equipment, Subsystems and Systems MIL-HDBK-244 Guid

ify that this is the current version before use. MIL-HDBK-419A To determine the true resistance of the earth electrode, X is allowed to assume convenient increments from zero to Ck. For each Ck, the value of measured resistance corresponding to the resultant P t (calculated with Equation 2-50) is read from the curves of Figure 2-18 and plotted against X. For example, if X and C k both equal 305 M (1000 feet), considering only the right hand curve in Figure 2-18, the value of Pt is 240, and R is 0.08 ohms. Next let X be 244 m (800 feet). The corresponding value of Pt is 96 m (316 feet) and r is 0.1 ohms. In this manner, estimates of the 62 percent values can be taken from Figure 2-18 and replotted as “true” resistance versus X, as shown in Figure 2-20. At the region of intersection of the c

ers (Part 1, Test Procedure: Part 2, Evaluation of Results). ATC 105 recognizes two methods for evaluating the performance of a cooling tower: the characteristic curve method and the performance curve method. Both methods require the same measured data and calculate the same performance parameter. The following are the major measurements which must be made. a) Wet bulb temperature at tower inlet. b) Dry bulb temperature. c) Cold water temperature. d) Hot water temperature. e) Cooling water flow. f) Fan power. INACTIVE MIL-HDBK-1003/7 244 g) Makeup water temperature. h) Makeup water flow. i) Blowdown temperature. j) Blowdown flow. As a result of calculations, the cooling tower capability can be quantified as a percent of design. 19.1.2.5 Evaporators. Evaporators shall be tested in accordanc