MIL-HDBK-274A
CONTENTS |
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PARAGRAPH |
PAGE |
|
FOREWORD |
ii |
|
1. SCOPE |
1 |
|
1.1 Purpose |
1 |
|
1.2 Background |
1 |
|
1.3 Structure |
1 |
2. |
APPLICABLE DOCUMENTS |
1 |
2.1 |
General |
1 |
2.2 |
Government documents |
1 |
2.3 |
Non-Government publications |
3 |
3. |
DEFINITIONS, ACRONYMS, AND ABBREVIATIONS |
4 |
3.1 |
Definitions |
4 |
3.2 |
Acronyms and abbreviations |
5 |
4. |
GENERAL GUIDANCE |
7 |
4.1 |
Theoretical basis for aircraft grounding |
7 |
4.2 |
Electrostatic theory |
7 |
4.3 |
Scenarios |
7 |
4.4 |
Energy sources |
7 |
4.4.1 |
Static energy sources |
8 |
4.4.2 |
Power |
14 |
4.4.3 |
Summary |
25 |
4.5 |
Airframe/personnel electrical parameters |
25 |
4.5.1 |
Electrostatic charge storage |
25 |
4.5.2 |
Electrical properties of aircraft |
26 |
4.5.3 |
Aircraft resistance |
26 |
4.5.4 |
Aircraft tire resistance |
26 |
4.5.5 |
Runway material |
26 |
4.5.6 |
Aircraft capacitance |
26 |
4.5.7 |
Human body electric parameters |
26 |
4.5.8 |
Aircraft or capacitor discharge |
27 |
4.5.9 |
Discoordination threshold levels |
27 |
4.6 |
Damage threshold levels |
27 |
4.6.1 |
Ordnance |
27 |
4.6.2 |
Sources of injury from shock |
27 |
iii
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