The development of optical techniques capable of measuring in-stream flow properties of air breathing hypersonic engines is a goal of the Aerospace Propulsion Division at AFRL. This goal is motivated by the need for in-stream data to support both ground and flight tests of scramjet engine designs. While particular fundamental hypersonic flow problems are addressable using well-established laser-based techniques, advanced engine concepts using axisymmetric hardware typically have minimal optical access making some of the more traditional techniques difficult to deploy. To meet the need we have an ongoing in-house program to mature diode-laser-based techniques for application in hypersonic flows. Additional motivation for developing diode-laser-based measurement strategies comes from the need for flight sensors. Flight-worthy packages must be small, light, low-power and rugged. For measurement objectives in both ground and flight experiments we have adopted tunable diode laser absorption spectroscopy making heavy use of fiber coupling and integrated optomechanics. Water-based measurements of temperature, pressure, velocity, and water mole fraction are executed using time-multiplexed near-infrared diodes. These fundamental flow parameters can be combined to yield optical mass capture and thrust. Similar measurements can be made in inlets using an oxygen-based strategy employing visible diodes. In this paper we summarize the absorption sensor work done to date in AFRL. Particular attention will be paid to the fact that a single hardware platform can be used to capture absorption, non-resonant transmission, and optical emission signals all three of which provide relevant information.