Traditionally, small satellites were launched by heavy launchers, as an additional payload, during missions to launch larger satellites. The unsuitability of this method, given the technical and financial constraints of a launch, and the growing demand for small satellite launches, have led to the development of small launchers.
Since the launch of small satellites via small launchers is still expensive for many companies and not optimised, the need to develop orbital transfer vehicles, with the potential to introduce an even greater differentiation in the cost of launching small satellites, has emerged.
However, to capture and maintain a significant market share, orbital transfer vehicles will need to enable for low-cost manufacturing and high flexibility in terms of mission profile and configuration. And that will require performant, simple, safe, reliable and restartable engines that allow thrust modulation over a wide range.