Artificial and Natural Icing Tests of the EH-60A Quick Fix Helicopter.
Artificial and natural icing flight tests were conducted on the EH-60A, Quick Fix helicopter (USA SN 84-24019) to establish a moderate icing flight envelope for the helicopter with the AN/ALQ-151(V)2 countermeasures system installed. The tests were conducted at Duluth, Minnesota from 24 February to...
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ftdtic:ADA204589 2023-05-15T16:37:25+02:00 Artificial and Natural Icing Tests of the EH-60A Quick Fix Helicopter. Lewis, William D. Hanks, Marvin L. Young, Christopher J. ARMY AVIATION ENGINEERING FLIGHT ACTIVITY EDWARDS AFB CA 1988-06 text/html http://www.dtic.mil/docs/citations/ADA204589 http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA204589 en eng http://www.dtic.mil/docs/citations/ADA204589 APPROVED FOR PUBLIC RELEASE DTIC AND NTIS Snow Ice and Permafrost Helicopters *HELICOPTERS *ICE FORMATION ACCUMULATION ANTENNAS ATMOSPHERIC TEMPERATURE DAMAGE DEFICIENCIES DIPOLE ANTENNAS DIRECTION FINDING ELECTRONIC COUNTERMEASURES ENGINES ENVIRONMENTS FLIGHT FLIGHT ENVELOPE FLIGHT TESTING ICE INLETS MINNESOTA OSCILLATION PROBES PROTECTION ROTORS TEST METHODS LPN-AEFA-88-06 EH-60A aircraft H-60 aircraft AN/ALQ-151 Text 1988 ftdtic 2016-02-19T11:27:22Z Artificial and natural icing flight tests were conducted on the EH-60A, Quick Fix helicopter (USA SN 84-24019) to establish a moderate icing flight envelope for the helicopter with the AN/ALQ-151(V)2 countermeasures system installed. The tests were conducted at Duluth, Minnesota from 24 February to 20 March 1988. A total of 11.8 flight hours were flown in the icing environment. After damage to an unprotected direction finding (DF) dipole antenna during an icing encounter, the project was terminated. During these tests, two deficiencies and eight shortcomings were noted. The two icing related deficiencies are: Excessive DF dipole antenna element oscillations induced by ice accumulation resulting in damage to the DF antenna element mounts and phenolic blocks, and the ice accretion and shedding characteristics of the EH-60A helicopter forward of the engine inlets resulting in a high probability of engine foreign object damage. The major shortcomings are: The excessive increase in power required with rotor system ice accumulation, the excessive Electronic Countermeasures (ECM) antenna oscillations induced by ice accumulation, the ice accretion and shedding characteristics of the outside air temperature probes, and the inability of the ECM antenna to fully retract following an icing flight. Four additional shortcomings were identified. The EH-60A Quick Fix helicopter, as configured for this test, was not suitable for flight into an icing environment. The EH-60A Quick Fix helicopter, as configured for this test, should not be cleared for flight in icing conditions. (sdw) Text Ice permafrost Defense Technical Information Center: DTIC Technical Reports database |
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Open Polar |
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Defense Technical Information Center: DTIC Technical Reports database |
op_collection_id |
ftdtic |
language |
English |
topic |
Snow Ice and Permafrost Helicopters *HELICOPTERS *ICE FORMATION ACCUMULATION ANTENNAS ATMOSPHERIC TEMPERATURE DAMAGE DEFICIENCIES DIPOLE ANTENNAS DIRECTION FINDING ELECTRONIC COUNTERMEASURES ENGINES ENVIRONMENTS FLIGHT FLIGHT ENVELOPE FLIGHT TESTING ICE INLETS MINNESOTA OSCILLATION PROBES PROTECTION ROTORS TEST METHODS LPN-AEFA-88-06 EH-60A aircraft H-60 aircraft AN/ALQ-151 |
spellingShingle |
Snow Ice and Permafrost Helicopters *HELICOPTERS *ICE FORMATION ACCUMULATION ANTENNAS ATMOSPHERIC TEMPERATURE DAMAGE DEFICIENCIES DIPOLE ANTENNAS DIRECTION FINDING ELECTRONIC COUNTERMEASURES ENGINES ENVIRONMENTS FLIGHT FLIGHT ENVELOPE FLIGHT TESTING ICE INLETS MINNESOTA OSCILLATION PROBES PROTECTION ROTORS TEST METHODS LPN-AEFA-88-06 EH-60A aircraft H-60 aircraft AN/ALQ-151 Lewis, William D. Hanks, Marvin L. Young, Christopher J. Artificial and Natural Icing Tests of the EH-60A Quick Fix Helicopter. |
topic_facet |
Snow Ice and Permafrost Helicopters *HELICOPTERS *ICE FORMATION ACCUMULATION ANTENNAS ATMOSPHERIC TEMPERATURE DAMAGE DEFICIENCIES DIPOLE ANTENNAS DIRECTION FINDING ELECTRONIC COUNTERMEASURES ENGINES ENVIRONMENTS FLIGHT FLIGHT ENVELOPE FLIGHT TESTING ICE INLETS MINNESOTA OSCILLATION PROBES PROTECTION ROTORS TEST METHODS LPN-AEFA-88-06 EH-60A aircraft H-60 aircraft AN/ALQ-151 |
description |
Artificial and natural icing flight tests were conducted on the EH-60A, Quick Fix helicopter (USA SN 84-24019) to establish a moderate icing flight envelope for the helicopter with the AN/ALQ-151(V)2 countermeasures system installed. The tests were conducted at Duluth, Minnesota from 24 February to 20 March 1988. A total of 11.8 flight hours were flown in the icing environment. After damage to an unprotected direction finding (DF) dipole antenna during an icing encounter, the project was terminated. During these tests, two deficiencies and eight shortcomings were noted. The two icing related deficiencies are: Excessive DF dipole antenna element oscillations induced by ice accumulation resulting in damage to the DF antenna element mounts and phenolic blocks, and the ice accretion and shedding characteristics of the EH-60A helicopter forward of the engine inlets resulting in a high probability of engine foreign object damage. The major shortcomings are: The excessive increase in power required with rotor system ice accumulation, the excessive Electronic Countermeasures (ECM) antenna oscillations induced by ice accumulation, the ice accretion and shedding characteristics of the outside air temperature probes, and the inability of the ECM antenna to fully retract following an icing flight. Four additional shortcomings were identified. The EH-60A Quick Fix helicopter, as configured for this test, was not suitable for flight into an icing environment. The EH-60A Quick Fix helicopter, as configured for this test, should not be cleared for flight in icing conditions. (sdw) |
author2 |
ARMY AVIATION ENGINEERING FLIGHT ACTIVITY EDWARDS AFB CA |
format |
Text |
author |
Lewis, William D. Hanks, Marvin L. Young, Christopher J. |
author_facet |
Lewis, William D. Hanks, Marvin L. Young, Christopher J. |
author_sort |
Lewis, William D. |
title |
Artificial and Natural Icing Tests of the EH-60A Quick Fix Helicopter. |
title_short |
Artificial and Natural Icing Tests of the EH-60A Quick Fix Helicopter. |
title_full |
Artificial and Natural Icing Tests of the EH-60A Quick Fix Helicopter. |
title_fullStr |
Artificial and Natural Icing Tests of the EH-60A Quick Fix Helicopter. |
title_full_unstemmed |
Artificial and Natural Icing Tests of the EH-60A Quick Fix Helicopter. |
title_sort |
artificial and natural icing tests of the eh-60a quick fix helicopter. |
publishDate |
1988 |
url |
http://www.dtic.mil/docs/citations/ADA204589 http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA204589 |
genre |
Ice permafrost |
genre_facet |
Ice permafrost |
op_source |
DTIC AND NTIS |
op_relation |
http://www.dtic.mil/docs/citations/ADA204589 |
op_rights |
APPROVED FOR PUBLIC RELEASE |
_version_ |
1766027714880339968 |