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Cricketsonde
A Cricketsonde (Cold Rocket Instrument Carrying Kit sonde) was a CO2 propelled, low-altitude meteorological rocket designed in the early 1960s by Texaco Inc. and the Friez Instrument Division of Bendix Corporation. It was used by various government and academic agencies until at least the late 1960s. The rocket carried what was essentially a radiosonde payload and was capable of reaching over 3000' (914 meter) altitude, where it then ejected a parachute and sent telemetry about temperature, humidity and barometric pressure on a frequency of 403 MHz during decent. A ground station with a manually tracked antenna received the signal where the data was processed and recorded.
== Vehicle Overview ==
The Cricketsonde rocket, made primarily of aluminum, was approximately 2.5 feet in length and 3 inches in diameter, and consisted of a propellant section, a recovery section, and a payload section. With the standard payload (telemetry package, battery and parachute), it weighed 5.5 lbs fully fueled.〔 Depending on payload weight, the cricketsonde could achieve altitudes of over 3700 feet (1127 meters).
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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