New configurations for the windshield and the canopy for a two-seater trainer military aircraft

Aircraft Engineering and Aerospace Technology

Volumn 75, Issue 2, 2003, Pages 156-163

  Lanciotti, Agostino ^a   Mantelli, Roberto ^b  

^a UNIVERSITY OF PISA   (Italy)

^b NONE

Author keywords

Aerospace engineering; Aircraft

Indexed keywords

AERODYNAMICS; AIRCRAFT MATERIALS; AIRCRAFT WINDSHIELDS; FUSELAGES; HINGES; MILITARY AIRCRAFT; ROTATION; TRAINING AIRCRAFT;

CANOPY; MILITARY TRAINER AIRCRAFT;

AEROSPACE ENGINEERING;

EID: 0037258855     PISSN: 00022667     EISSN: None     Source Type: Journal    
DOI: 10.1108/00022660310465771     Document Type: Article

References (5)

1. Anon. Military Specification (1974), General specification for cockpit canopy system, fixed wing single and multiplace, fighter, attack, and trainer aircraft. MIL-C-81590.
2. Anon. Military Specification (1988), General specification for Windshield systems, fixed wing aircraft. MIL-W-81752A.
3. Anon. Military Specification (1988), Plastic sheet, acrylic, modified. MIL-P-8184.
4. Belyakov, R.A. and Marmain, J (1994), MIG 1939-1989, Edition Lariviere.
5. Taylor, G. (1980), JANE'S all the World Aircraft, Jane's Publishing Comp., London.