Future space missions such as IXO would benefit from a pulse tube cooler providing several hundreds milliwatts of cooling power at 15 K for the pre cooling of a Joule Thomson loop. Our team, in partnership with Air Liquide and Thales Cryogenics BV, is involved in the development of such a product in the framework of an ESA contract. The goal is the development of an engineering model of a 3 stage pulse tube. Our approach is based on multistage pulse tube thermally linked together. This modular approach allows for more flexibility in the mechanical design while keeping a high thermal efficiency. Our first experimental results with performances below 15 K are described. A preliminary structure for a 3 stage pulse tube reaching 15 K is presented.