| Presently, NASA is designing a replacement for its existing satellite laser ranging systems. These systems are used to measure Earth-satellite distances, tectonic plate movement, variations in rotational motion and other geodetic phenomena. Satellite Laser Ranging 2000 (SLR2000) is envisioned as a fully automated, sub-centimeter accuracy, eye-safe, low-cost replacement to the current SLR systems. It is expected to overcome present limitations by operating autonomously; being free of optical, chemical or electrical hazards; and having a greater average time between failures. Expected shot range precision is about one centimeter with normal point precision of better than three centimeters. This system will have twenty-four hour tracking coverage. SLR2000 specifications dictate operation at visible wavelengths with eye-safe energies on the order of one hundred microjoules and repetition rates on the order of two kilohertz.; The optical subsystem of SLR2000 includes a passively Q-switched Nd:YAG microlaser. Passive Q-switching will be achieved using a saturable absorber and offers a number of advantages over the mode-locked lasers currently used in ranging stations: no need for long resonators with tight thermal control; no electro-optic switch required for single pulse selection; saturable absorbers precluding the use of carcinogenic dyes and solvents; and RF drive frequency electronics not tied to the resonator length of the laser cavity. The presented work describes the research and development of a prototype laser used to produce the energies, repetition rates and pulsewidths required for SLR2000. Optimization theories and models were applied to the laser design in order to accurately predict and assess performance characteristics of both gain medium and saturable absorber. Data were obtained which illustrated the affect of pump laser saturation and thermal lensing of the gain medium. Important laboratory skills and techniques were acquired in the design and construction of passively Q-switched microlasers. |
