AH-1 Helicopter Vibration Levels for Stub Wing Mounted Equipment.

Welford, Gordon D.; Boland, Joseph S., Iii

AH-1 Helicopter Vibration Levels for Stub Wing Mounted Equipment.

Active / Technical Report | Accession Number: ADA026825 |

Need Help?

Abstract:

This report presents measured translational and angular acceleration inputs to stub wing mounted equipment on the AH-1 helicopter. In this case the wing mounted electro-optical systems were the stabilized platform airborne laser system and the stabilized mirror airborne laser system. The data are presented in the form of power spectral density, amplitude versus frequency, and oscillograph charts.

Author(s):

Welford, Gordon D. ; Boland, Joseph S., Iii

Author Organization(s):

ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL ALA GUIDANCE AND CONTROL DIRECTORATE

Descriptive Note:

Technical rept.,

Pagination:

0147

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:

Approved For Public Release

RECORD

Collection: TR

Identifying Numbers

Report Number(s):

RG-76-30

Subject Terms

Communities of Interest:

Air Platforms

Descriptor(s):

*LASER TARGET DESIGNATORS, *HELICOPTERS, *AIRCRAFT PROTUBERANCES, VIBRATION, POWER SPECTRA, STABILIZED PLATFORMS, VIBRATIONAL SPECTRA, LASER TRACKING

Field(s)/Group(s):

Helicopters

Keyword(s):

H 1 aircraft, AH 1 aircraft, Huey Cobra

Report Date:

1975 Sep 01