MIL-PRF-7032 Revision H:2010
Current
The latest, up-to-date edition.
Inverters, Aircraft, General Specification for
10-09-2010
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Specifies the general requirements for inverters that convert electrical power in aircraft from nominal 28 volts direct current (VDC) power to three-phase or single-phase alternating current (AC) power at 400 hertz.
| DevelopmentNote |
Supersedes MIL I 7032 (G). (09/2010) Supersedes MIL I 85071. (10/2010) H NOTICE 1 - Notice of Validation. (09/2016) NEW CHILD NOT 2 2021 IS NOW ADDED
|
| DocumentType |
Standard
|
| Pages |
53
|
| ProductNote |
NEW CHILD NOT 2 2021 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
This specification establishes the general requirements for inverters that convert electrical power in aircraft from nominal 28 volts direct current (VDC) (see 6.5.4) power to three-phase or single-phase alternating current (AC) (see 6.5.2) power at 400 hertz.
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