Titanium (Ti) and the alloy Ti-6Al-4V (Ti64) possess material properties of great value to the aerospace industry, such as a superior strength to weight ratio, resistance to corrosion and fracture toughness. Ti alloys are compatible with composite materials, possessing a similar thermal expansion. There is therefore a global effort to utilise additively manufactured (AM) Ti64 in aircraft. However, there is a lack of high quality equation of state (EoS) and strength data for Ti and Ti64. There is no data at all on AM Ti64. Without adequate data to improve models, it is not possible to reduce design uncertainties and optimise aircraft performance. We propose to address this deficiency by studying the structural, microstructural and elastic properties of commercial Ti and commercial and AM Ti64 up to 35 GPa and 1500 K at ID06 LVP by simultaneously collecting X-ray diffraction patterns, X-ray images, and pulse-echo ultrasonic data.