X-15A-2高超声速飞行中增加的驾驶任务和性能

IF 1.4 4区 工程技术 Q2 ENGINEERING, AEROSPACE
WM. J. “Pete” Knight
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引用次数: 0

摘要

在过去的几年里,驾驶一架基本的X-15从发射到以精确的速度和高度着陆被认为是一项要求很高的驾驶任务。每次任务的成功取决于飞行员在高马赫数、高加速度、高海拔和极限温度的敌对飞行环境中飞行的生理和心理压力下的表现能力。今天,飞机已经进行了广泛的修改,以使X-15成为冲压发动机的测试平台飞行器,它将取代可移动的腹侧,为测试和开发用于未来高超音速巡航飞行器的可操作原型冲压发动机提供实时飞行环境。图1所示的附加系统(外部燃料箱、冲压发动机、外部窗口和烧蚀涂层)及其相关的应急程序和X-15A-2的飞行特性下降,大大增加了飞行员的工作量,超过了标准的X-15任务。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Increased Piloting Tasks and Performance of X-15A-2 in Hypersonic Flight
In past years, flying a basic X-15 from launch through a dead stick landing on a precise speed and altitude profile was considered a demanding piloting task. The success of each mission was determined by the pilot's ability to perform under the physiological and psychological stresses of flight into a hostile flight environment of high Mach numbers, high accelerations, high altitude, and limiting temperatures. Today the aircraft has been extensively modified to qualify the X-15 as a test bed vehicle for a ramjet engine, which will be carried in place of the movable ventral, providing real time flight environment for testing and developing an operational prototype ramjet for use on future hypersonic cruise vehicles. The additional systems pictured in Fig. 1 (external tanks, ramjet, external window, and ablative coating), their associated emergency procedures and the degraded flying characteristics of the X-15A-2 have increased the pilot's workload significantly over the standard X-15 mission.
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来源期刊
Aeronautical Journal
Aeronautical Journal 工程技术-工程:宇航
CiteScore
3.70
自引率
14.30%
发文量
86
审稿时长
6-12 weeks
期刊介绍: The Aeronautical Journal contains original papers on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are therefore solicited on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are also welcomed which review, comprehensively, the results of recent research developments in any of the above topics.
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