1. AIAA 99-2600 Development status of the VINCI engine for Ariane 5upper stage F. Jean-J.L.Barthoulot (SNECMA)
2. AIAA 99-2191 Design of a high performance low hydrogen turbopump forVINCI engine R.Bosson -B. Goirand (SNECMA) cost
3. AIAA 99-2601 Development of the thrust chamber forthe new cryogenic upper stage engine forAriane T.Mattstedt -F.Haidinger -C.Hensel (DASA)
4. AIAA 99-2474 Ignition System Concept forthe new Cryogenic Upper Stage Engine of Ariane 5 C. Hensel -T. Mattstedt -W.Oechslein (DASA) E. Vermeulen-M. DeWilde (SPE)