Gurkin L W
Sounding Rockets Projects Branch, NASA/Goddard Space Flight Center, Wallops Flight Facility, Wallops Island, Virginia 23337, USA.
ASGSB Bull. 1992 Oct;6(1):113-20.
High altitude suborbital rockets (sounding rockets) have been extensively used for space science research in the post-World War II period; the NASA Sounding Rocket Program has been on-going since the inception of the Agency and supports all space science disciplines. In recent years, sounding rockets have been utilized to provide a low gravity environment for materials processing research, particularly in the commercial sector. Sounding rockets offer unique features as a low gravity flight platform. Quick response and low cost combine to provide more frequent spaceflight opportunities. Suborbital spacecraft design practice has achieved a high level of sophistication which optimizes the limited available flight times. High data-rate telemetry, real-time ground up-link command and down-link video data are routinely used in sounding rocket payloads. Standard, off-the-shelf, active control systems are available which limit payload body rates such that the gravitational environment remains less than 10(-4) g during the control period. Operational launch vehicles are available which can provide up to 7 minutes of experiment time for experiment weights up to 270 kg. Standard payload recovery systems allow soft impact retrieval of payloads. When launched from White Sands Missile Range, New Mexico, payloads can be retrieved and returned to the launch site within hours.
高海拔亚轨道火箭(探空火箭)在二战后被广泛用于空间科学研究;美国国家航空航天局(NASA)的探空火箭计划自该机构成立以来一直在进行,并支持所有空间科学学科。近年来,探空火箭已被用于为材料加工研究提供低重力环境,特别是在商业领域。探空火箭作为一种低重力飞行平台具有独特的特点。快速响应和低成本相结合,提供了更频繁的太空飞行机会。亚轨道航天器设计实践已达到高度复杂的水平,优化了有限的可用飞行时间。高数据率遥测、实时地面上行链路指令和下行链路视频数据通常用于探空火箭有效载荷。现有的标准现货主动控制系统可限制有效载荷的机体速率,使控制期间的重力环境保持在10^(-4)g以下。现有的可操作运载火箭可为重达270千克的实验提供长达7分钟的实验时间。标准的有效载荷回收系统允许对有效载荷进行软着陆回收。从新墨西哥州白沙导弹靶场发射时,有效载荷可在数小时内被找回并返回发射场。