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Attachment B: Copyrighted Literature Search Results - FAA Human ...

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AA- AD-B095 681/3<br />

TI- Data Presentation from Air-to-Air Combat Maneuvering between an S-76<br />

and a UH-60A<br />

TI- Technical rept<br />

AU- Wolfrom, J. A. ; Fisher, C. E.<br />

CS- Army Aviation Systems Command, St. Louis, MO.<br />

CS- 027529000; 404318<br />

RN- USAAVSCOM-TR-85-D-17<br />

PY- Sep 85<br />

PG- 124p<br />

NT- Distribution limitation now removed. Order this product from NTIS by:<br />

phone at 1-800-553-NTIS (U.S. customers); (703)605-6000 (other<br />

countries); fax at (703)321-8547; and email at<br />

orders@ntis.fedworld.gov. NTIS is located at 5285 Port Royal Road,<br />

Springfield, VA, 22161, USA.<br />

LA- English<br />

PC- PC A07/MF A02<br />

JA- GRAI9709<br />

CP- United States<br />

AB- This report presents data measured during one-on-one air-to-air<br />

maneuvering tests involving Army UH-60A and Sikorsky S-76 helicompters.<br />

The engagements included preplanned manuevering engagements as well as<br />

unstructured engagements in which both helicopters were maneuvered<br />

agressively to gain a tactical advantage. The test program was<br />

conducted during July 1983 a the Naval Air Test Center, Patuxent River,<br />

Maryland, and included the OH-58A in addition to the two helicopters<br />

mentioned above. This report contains data only on the S-76 and UH-60A;<br />

data from the OH-58A has been published in two separate reports. The<br />

data for each helicopter are presented in the form of time histories of<br />

the various parameters of the various parameters as measured during the<br />

maneuvers. The parameters for which data are presented include aircraft<br />

position in space, pitch, roll, and sideslip attitueds; pitch, roll,<br />

and yaw rates; control positions; load factor; airspeed; rotor speed;<br />

altitude; and engine torque. In addition to the tie histories, several<br />

of the parameters are cross-plotted using time as the associating<br />

variable. These cross-plots permit a ready assessment of the flight<br />

envelope utilized by each helicopter during the air combat maneuvering.<br />

Originator-supplied keywords: Maneuverability; Agility; Air-to-Air<br />

combat; Manuevers; Flight testing; and Data acquisition and<br />

instrumentation.<br />

DE- *Flight maneuvers; *Aerial warfare; *Helicopters; Aircraft; Airspeed;<br />

Data acquisition; Engines; Flight envelope; Flight testing; History;<br />

Loads(Forces); Maneuverability; Position(Location); Rates; Rotors;<br />

Sideslip; Time; Torque; Yaw; Instrumentation; Army aircraft<br />

B-395<br />

ID- Uh-60a aircraft; H-60 aircraft; S-76 aircraft; NTISDODXA<br />

SH- 74G (Military Sciences--Military Operations, Strategy, and Tactics);<br />

51C (Aeronautics and Aerodynamics--Aircraft)<br />

AZ- 1993368<br />

AA- AD-A319 150/9<br />

TI- RAH-66 Comanche Health Hazard and Performance Issues for the Helmet<br />

Integrated Display and Sighting System<br />

TI- Final rept<br />

AU- Rash, C. E. ; Mozo, B. T. ; McEntire, B. J. ; Licina, J. R.<br />

CS- Army Aeromedical Research Lab., Fort Rucker, AL.<br />

CS- 026909000; 404578<br />

RN- USAARL-97-1<br />

CN- 3M162787A879<br />

PY- Nov 96<br />

PG- 48p<br />

NT- Product reproduced from digital image. Order this product from NTIS by:<br />

phone at 1-800-553-NTIS (U.S. customers); (703)605-6000 (other<br />

countries); fax at (703)321-8547; and email at<br />

orders@ntis.fedworld.gov. NTIS is located at 5285 Port Royal Road,<br />

Springfield, VA, 22161, USA.<br />

LA- English<br />

PC- PC A04/MF A01<br />

JA- GRAI9709<br />

CP- United States<br />

AB- The helmet integrated and display sighting system (HIDSS) is a<br />

combination of a protective helmet, helmet mounted display (HMD), and<br />

helmet mounted sighting system. It is planned for use in the Army's<br />

next generation reconnaissance/attack helicopter, the RAH-66 Comanche.<br />

In 1986 and 1988, USAARL developed and published guidelines for<br />

addressing potential health hazard issues with the HIDSS. The most<br />

recent version of these guidelines was USAARL LR 88-4-21-1O, 'Revision<br />

for the health hazard issues in the MIDSS.' This paper is a further<br />

revision of these issues. In addition to recommendations provided for<br />

performance in the areas of biodynamics, optics/vision, and acoustics,<br />

a number of safety and training issues are discussed.<br />

DE- *Attack helicopters; *Aircraft equipment; *Helmet mounted displays;<br />

Optics; Integrated systems; Hazards; Health; Safety; Acoustics;<br />

Protective clothing; Reconnaissance aircraft; Flight helmets;<br />

Biodynamics<br />

ID- *Health hazards; Rah-66 aircraft; Hidss(Helmet integrated and display<br />

sighting system); NTISDODXA<br />

SH- 51C (Aeronautics and Aerodynamics--Aircraft); 49E

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