Advanced manufacturing of titanium propellant tanks for space applications part 1: tank design and demonstrator manufacturing

Author:

Norman A. F.ORCID,Iqbal N.,Robelou A.,Nor K.,Andrews D.,Martin J.,Dodds S.,Bellarosa R.,Meisnar M.,Ghidini T.

Funder

European Space Agency

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference26 articles.

1. ECSS Structural materials handbook–Part 5: new advanced materials, advanced metallic materials, general design aspects and load transfer and design of joints, ECSS-E-HB-32-20 Part 5A, March 2011

2. Bellarosa, R: Trade-off of Al–Li for spacecraft propellant tanks (requirements specification) 2014. Airbus Defence and Space. Restricted access

3. Uney, P.E., Fester D.A.: Material compatibility with space storable propellants—design guidebook, Jet Propulsion Laboratory, Pasadena, California, 1972

4. Bellarosa, R., Catherall, D.: Airbus defence and space eurostar spacecraft propellant tanks past, present and future. In: Space propulsion conference, Cologne, May 2014

5. Sylva G.D., Christener B.K.: Development of low cost, short lead time, satellite propellant tank using Ti15333, Titanium 95, Science and Technology, p. 612

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