Cincinnati, OH, June 11-13, 1984. 11 p. Research supported by the Centre National d'Etudes Spatiales. Report No.: AIAA PAPER 84—1226 Language: Eng1ish. Country of Origin: France. Country of Publication: United States Document Type: PREPRINT Most documents avai1ab1e from AIAA Technica1 Library J o u r n a 1 A n n o u n c e m e n t s IA A 8 417 The mission goals and initial design parameters for a prospective Ariane 5 rocket are discussed. The Ariane 5 would be a heavy lift launch vehicle capable of placing up to 3000 kg in GEO, 4000 kg satellites in sun- synchronous orbits, 15 ton space station modules and specialized units into LEO and launching the mini-Shuttle Hermes. Fairings will be increased to 10 m for Shuttledensity loads. An expendable launcher with a reusable third stage and a variable purpose upper stage is under consideration. The continued usage of cryogenic fuels and the HM60 engine is regarded as essentia1 for meeting cost goals. First flight of the Ariane 5 is envisioned for 1995. (M.S.K.) Source of Abstract (Subfi1e): AIAA/TIS Descriptors: *ARIANE LAUNCH VEHICLE; *LAUNCH VEHICLE CONFIBURATIONS; *PR0PULSION SYSTEM CONFIGURATIONS; COMMERCIAL SPACECRAFT; CRYOGENIC ROCKET PROPELLANTS; PAYLOAD MASS RATIO; SPACECRAFT POWER SUPPLIES; UPPER STAGE ROCKET ENGINES Subject Classification: 7515 Launch Vehicles & Space? Vehicles (1975-) Design of a project plan for the establishment of a lunar factory. ENTWURF EINES PROJEKTPLANES FUER DIE ERRICHTUNG EINER MONDI-ABRIK. KOELLE, H. H. ; THOMAS, U.; APEL, U.; BALZER, R.; BERNAU, D. ; CZARNITZKI, J.; GINAT I, A.; HEIDEN, 0.; RYBA , J.; SCHULZ, B. Techoi sche Univ., Berlin (West Germany). Fachgebeit R a u m f a h r 11 e c h n i k . Corp. Source Code: TJ477159 Aug. 1983. 58P. Report No.: ILR-MITT-123 Language: MULTIPLE. In GERMAN; ENGLISH summary Country of 0rigin: Germany , Federa1 Repub1ic of. Country of Publication: Germany, Federal Republic of Document Type: REPORT Most documents avai1ab1e from AIAA Technica1 Library Other Availability: NT IS HC A04/MF A01 J our rial Announcement: STAR8410 A project for a lunar factory producing feedstock and constructi on material for the manufacturi ng of space solar power plants, and large quantities of liquid oxygen for propulsion is outlined. A systems description, a time schedule, a cost plan and a proposal for an organization to carry out such a project are presented. Benefits and risks are discussed. It is shown that such a
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