A conceptual design study of the ARIM-1 sounding rocket mission, whose goal is to study atmospheric turbulence in the tropopause region of the atmosphere, is presented. The implementation of the ARIM-1 mission will be carried out by students participating in the Alaska Student Rocket Program (ASRP), with a projected launch date of August 1997. Emphasis is placed on standardization of payload support systems. The thermosonde payload will measure the atmospheric turbulence by direct measurement of the temperature difference over a distance of one meter using two 3.45-micron 'hot-wire' probes. This document discusses the science objectives, mission analysis, payload mechanical configuration and structural design, recovery system, payload electronics, ground station, testing plans, and mission implementation.
ARIM-1: The Atmospheric Refractive Index Measurements Sounding Rocket Mission
1995
142 pages
Report
No indication
English
Aeronomy , Meteorological Instruments & Instrument Platforms , Atmospheric turbulence , Mission planning , Single stage rocket vehicles , Sounding rockets , Tropopause , Rocket sounding , Temperature measuring instruments , Hot-wire flowmeters , Payload integration , Recovery parachutes , Structural design , Temperature measurement
NTIS | 1998
|NTRS | 1998
|MASER-12 Sounding Rocket: A Hot Mission in Cold Environment
TIBKAT | 2013
|