1[1]Webb JT, Pilmanis AA .Impact of recent altitude physiology research on design of cockpit pressurization system. Proceedings of SAFE 35 th Annual Symposium, Phoenix,Arizona,1997.425-430
2[2]Self BP, Pilmanis AA, Diesel D. Extended exposure capability after rapid decompression at 60 000 feet and above. Proceedings of SAFE 35 th Annual Symposium, Phoenix,Arizona, 1997.431-436
3[3]Landervik B. Development of the Swedish tactical flight combat suit(TFCS). Proceedings of SAFE 33 th Annual Symposium. Reno, Nevada, SAFE Asoocciation, 1995.369-375
4[4]Lovett NP, Ashdown R. Development of the OBOGS and BRAG valve for the F-22 life support system. Proceedings of SAFE 36 th Annual Symposium. Phoenix, Arizona: SAFE Association, 1998.62-71
7[7]Ernsting J, Miller R. Advanced oxygen system for aircraft. North Atlantic Treaty Organization. Neuilly-Sur-Seine,France:Canada Communication Group, 1996.21-33
8[8]Marotte H, Gutman G. Modern pneumatic technology and the challenges of physiological protection for the pilot of advanced fighter aircraft. 28 th SAFE annual Symposium. Phoenix, Arizona, SAFE Association, 1991.47-52
9[9]Contarino,RN, Johnson BE. A solid state oxygen monitor for the on board oxygen generating system.31 th Annual Symposium.Las Vegas,Nevada: SAFE Association NOV 8- 10,1993.136-146
10[10]Shams T, Zhao Y ,Fullerton J. Interaction between computer models of face and mask. In:Proceedings of SAFE 35 th Annual Symposium. Phoenik, Arizona, SAFE Asoocciation, 1997.196-208
