The Nike-Cajun Sounding Rocket

L. M. Jones, W. Hansen, N. Spencer, W. Stroud, W. Berning
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Abstract

The Nike-Cajun all solid propellant sounding rocket is a two-stage combination, using the Nike booster as first stage and the Cajun as the instrument-carrying second stage. When fired at 85 deg launching angle and with a 15sec coast between stages, it has carried 50 lb to 100 miles altitude. Successful flights at Wallops Island, White Sands, Fort Churchill, and aboard ship have demonstrated that it is a simple and reliable sounding vehicle. It will be used during the IGY at Fort Churchill and at Guam. About 50 Nike-Cajuns will be instrumented to measure water-vapor distribution, the earth's magnetic field, cloud structure, pressure, temperature, density, winds, cosmic rays, and auroral particles.
耐克-卡津探空火箭
Nike-Cajun全固体推进剂探空火箭是一个两级组合,使用Nike助推器作为第一级,Cajun作为携带仪器的第二级。当以85度发射角发射,级间间隔15秒时,它可以携带50磅到100英里的高度。在沃洛普斯岛、白沙、丘吉尔堡和船上的成功飞行表明,它是一种简单可靠的测深工具。它将在丘吉尔堡和关岛的IGY期间使用。大约50台Nike-Cajuns将用于测量水蒸气分布、地球磁场、云结构、压力、温度、密度、风、宇宙射线和极光粒子。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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