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Gurkin, L. W.

Publications and source records attributed to Gurkin, L. W..

The NASA Sounding Rocket Program and space sciences

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.

Flight Experiment

Development and flight tests of a new middle atmosphere electric field payload

There has been a marked increase of scientific interest in middle atmosphere electrodynamics in recent years. This region, which encompasses the stratosphere and mesosphere, has generally been considered relatively passive, electrically. Attempts at in-situ electric field measurements throughout this region can only be accomplished by the use of sounding rockets. A series of middle atmosphere electrodynamic rocket flights have been conducted using a new electric field subpayload. This new payload is capable of measuring all three components of the vector electric field using the symmetric double probe technique. In six flight attempts, the subpayload has performed well and obtained E-field data on five flights. It has been successfully utilized in a mother-daughter configuration and as a stand-alone payload. The flight results have established the existence of large mesospheric electric fields, supporting previous results from single axis measurements.

Gurkin, L. W.

The International Ozone Intercomparison Program

The World Meteorological Organization (WMO) has endorsed a number of intercomparison project activities in recent years as a part of its Global Ozone Research and Monitoring Project. The present investigation is concerned with an intercomparison of rocket borne measurement techniques in continuation of that overall effort. The objectives of this investigation were to compare the performance of rocket borne instruments, via a set of simultaneous intercomparisons of various rocket instruments under at least two sets of conditions. In order to accomplish the objectives and to aid in validating the historical data, six daytime sensors from each participant were flown. In addition, two of the participants (Australia and U.S.) provided nighttime sensor measurements. Attention is given to Wallops Flight Center instrumentation and launch support, the Triad Series, The Morning Series, and the Nighttime Series.

Gurkin, L. W.

Performance enhancement of existing two-stage sounding rocket vehicles through the use of tandem booster systems

The three-stage Taurus-Nike-Tomahawk launch vehicle is being considered for performance enhancement of the existing Taurus-Tomahawk flight system. In addition, performance enhancement of other existing two-stage launch vehicles is being considered through the use of tandem booster systems. Aeroballistic characteristics of the proposed Taurus-Nike-Tomahawk vehicle are presented, as are overall performance capabilities of other potential three-stage flight systems.

Flores, C. C.