Optical measurement techniques are required to determine flow-field parameters for the development and evaluation of advanced combustion systems. Parameters include but are not limited to velocity, temperature, and species concentrations. There are many challenges to implementing diagnostic techniques in practical combustion rigs, including temperature/pressure effects, vibration, flow perturbation, limited optical access, as well as optical engineering and alignment. Current implementation options discussed here include incorporating in-situ launching assemblies and integrating fiber-based methods. First, a novel laser launching system is described for high-temperature, high-pressure combustion applications in the High-Pressure Combustion Research Facility (HPCRF) at Wright-Patterson AFB. This insitu, optical-based assembly is placed upstream in the plenum section of a combustor sector rig and used to launch double-pulsed laser light for particle-image velocimetry (PIV). Design and implementation challenges will be discussed and representative data shown. In addition to launching capability, this assembly provides the means for light collection. Optical designs will be discussed for coupling scattered light or fluorescence photons from sheet-based techniques such as PIV or planar laser-induced fluorescence (PLIF) to double-frame, high-speed, intensified cameras. Investigations into the use of this assembly for PLIF in reacting flows will be presented. Second, fiber-based approaches involving a novel imaging fiber and associated purged, watercooled probe for high-speed imaging of practical combusting flows in the HPCRF with CMOSbased cameras will be discussed. Together these two approaches represent a powerful methodology for bringing the advantages of nonintrusive, optical combustion diagnostics to practical hardware in large-scale combustion test facilities. Nomenclature HPCRF = high-pressure combustion research facility LAS = laser absorption spectroscopy PIV = particle-image velocimetry PLIF = planar laser-induced fluorescence TDM = time-division-multiplexed TVC = trapped vortex combustion UCC = ultra compact combustors WPAFB = Wright-Patterson Air Force base