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Rosetta Lander—Philae: Implications of an alternative mission
DOI: 10.1016/j.actaastro.2005.12.009 Bibcode: 2006AcAau..58..435U

Rosenbauer, H.; Hilchenbach, M.; Ulamec, S. +5 more

“Rosetta” is a Cornerstone Mission of the Horizon 2000 ESA Programme. Its goal is to rendezvous with a comet and to study its nucleus and coma using an orbiting spacecraft and a landed platform. The latter is called Philae; the Rosetta Lander has been designed to land softly on the comet nucleus and is equipped with 10 scientific instruments to pe…

2006 Acta Astronautica
Rosetta 22
Mission operations for the new Rosetta
DOI: 10.1016/j.actaastro.2005.06.003 Bibcode: 2006AcAau..58..105F

Ferri, Paolo

The International Rosetta Mission, a cornerstone mission of the European Space Agency Scientific Programme, was scheduled for launch in January 2003 on Ariane 5, but it missed its 19 days launch window due to the suspension of Ariane 5 launches following the failure of flight 517 in December 2002. The search for a new mission opportunity started i…

2006 Acta Astronautica
Rosetta 18
Rosetta on its way to the outer solar system
DOI: 10.1016/j.actaastro.2006.02.024 Bibcode: 2006AcAau..59..301M

Montagnon, Elsa; Ferri, Paolo

The International Rosetta Mission, a cornerstone mission of the European Space Agency Scientific Programme, was launched on 2nd March 2004 on its 10 years journey towards a rendezvous with comet Churyumov Gerasimenko. Once reached the comet nucleus in summer 2014, Rosetta will orbit it for about 1.5 years down to distances of a few kilometers and …

2006 Acta Astronautica
Rosetta 11
SMA gas release mechanism for the Rosetta Lander's Ptolemy instrument
DOI: 10.1016/j.actaastro.2006.01.015 Bibcode: 2006AcAau..58..576E

Sawyer, Eric; Edeson, Ruben; Whalley, Martin +2 more

The Ptolemy instrument on the Rosetta comet lander “Philae” is an advanced gas analyser. The instrument relies on a supply of ultra-clean helium gas to carry cometary matter through a series of gas chromatography columns and high temperature reactors, into a mass spectrometer. The helium is stored in a pair of titanium gas tanks, pressurised to 50…

2006 Acta Astronautica
Rosetta 4
Cassini/Huygens at Saturn and Titan
DOI: 10.1016/j.actaastro.2006.02.040 Bibcode: 2006AcAau..59..335M

Mitchell, Robert T.

The Cassini/Huygens Project is a joint undertaking between NASA, the European Space Agency, and the Italian Space Agency to conduct an in-depth exploration of the Saturnian system. The spacecraft consists of an orbiter vehicle and an atmospheric probe which has completed its mission in the atmosphere and on the surface of Titan, the largest moon o…

2006 Acta Astronautica
Huygens 3
The Huygens probe—space history in many ways
DOI: 10.1016/j.actaastro.2006.02.046 Bibcode: 2006AcAau..59..319S

Lebreton, Jean-Pierre; Schipper, Anne Marie

The European Space Agency's Huygens probe, developed under the prime contractorship of Alcatel Alenia Space, has on the 14th January 2005 arrived at its final destination, Saturn's largest Moon Titan. This event provides a major step in our solar system exploration activities and represents a significant contribution to the exploration of Titan, a…

2006 Acta Astronautica
Huygens 2
Low cost development for the Rosetta Lander French subsystems: Lessons learned
DOI: 10.1016/j.actaastro.2005.07.009 Bibcode: 2006AcAau..59..661D

Debus, Andre; Moura, Denis

After the delay of the Rosetta mission launch, previously planned in January 2003, this mission, led by ESA, will finally be launched from Kourou by Ariane V G+ at the beginning of next year (2004). After a long trip, the spacecraft will reach the comet Churyumov Gerasimenko in 2014. The mission includes a lander, built by an European consortium u…

2006 Acta Astronautica
Rosetta 0
On the concepts of a highly integrated payload suite for use in future planetary missions: The example of the BepiColombo Mercury planetary orbiter
DOI: 10.1016/j.actaastro.2005.07.016 Bibcode: 2006AcAau..59..823K

Schulz, R.; Erd, C.; Buis, E. J. +6 more

Future low resource payload concepts will need to be developed from the viewpoint of a standard integrated payload suite where resources are dramatically reduced through high levels of integration and resource sharing. The study of this approach, its gains together with its limitations was the key objective of this work. The highly compact integra…

2006 Acta Astronautica
Rosetta SMART-1 0