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Proceedings of SPIE | 2004

SPECS: the kilometer-baseline far-IR interferometer in NASA's space science roadmap

David T. Leisawitz; Tom Abel; Ronald J. Allen; Dominic J. Benford; A. W. Blain; Claudio Bombardelli; Daniela Calzetti; Michael DiPirro; Pascale Ehrenfreund; Neal J. Evans; J. Fischer; Martin Harwit; Tristram T. Hyde; Marc J. Kuchner; Jesse Leitner; Enrico C. Lorenzini; John C. Mather; K. M. Menten; S. H. Moseley; Lee G. Mundy; Takao Nakagawa; David A. Neufeld; John C. Pearson; Stephen A. Rinehart; Juan Roman; Shobita Satyapal; R. F. Silverberg; H. Philip Stahl; Mark R. Swain; Theodore D. Swanson

Ultimately, after the Single Aperture Far-IR (SAFIR) telescope, astrophysicists will need a far-IR observatory that provides angular resolution comparable to that of the Hubble Space Telescope. At such resolution galaxies at high redshift, protostars, and nascent planetary systems will be resolved, and theoretical models for galaxy, star, and planet formation and evolution can be subjected to important observational tests. This paper updates information provided in a 2000 SPIE paper on the scientific motivation and design concepts for interferometric missions SPIRIT (the Space Infrared Interferometric Telescope) and SPECS (the Submillimeter Probe of the Evolution of Cosmic Structure). SPECS is a kilometer baseline far-IR/submillimeter imaging and spectral interferometer that depends on formation flying, and SPIRIT is a highly-capable pathfinder interferometer on a boom with a maximum baseline in the 30 - 50 m range. We describe recent community planning activities, remind readers of the scientific rationale for space-based far-infrared imaging interferometry, present updated design concepts for the SPIRIT and SPECS missions, and describe the main issues currently under study. The engineering and technology requirements for SPIRIT and SPECS, additional design details, recent technology developments, and technology roadmaps are given in a companion paper in the Proceedings of the conference on New Frontiers in Stellar Interferometry.


A CENTURY OF RELATIVITY PHYSICS: ERE 2005; XXVIII Spanish Relativity Meeting | 2006

Detector Configurations for Equivalence Principle Tests with Strong Separation of Signal from Noise

Enrico C. Lorenzini; I. I. Shapiro; Joshua Ashenberg; Claudio Bombardelli; P. N. Cheimets; V. Iafolla; D. M. Lucchesi; S. Nozzoli; F. Santoli; S.L. Glashow

Testing the Equivalence Principle (EP) at a level of accuracy substantially higher than the present state of the art requires resolving a very small signal out of the instrument’s intrinsic noise and also the noise associated with the instrument’s motion and gravity gradients. In the test of the Equivalence Principle in an Einstein Elevator under development by our team, the acceleration detector spins about a horizontal axis while free falling for about 25 s inside a co‐moving capsule released from a stratospheric balloon. The characteristics of the instrument package and the configuration of the detector play a key role in the ability to extract an EP violation signal at the desired threshold level out of dynamics‐related noise. Numerical simulations of the detector’s dynamics in the presence of relevant perturbations, having assumed realistic errors and construction imperfections, show the merits of the detector configuration selected. The results illustrate that the effects of dynamics and gravity gra...


AIAA Guidance, Navigation, and Control (GNC) Conference | 2013

GNC Design for Asteroid Orbit Modification Missions

Miguel Hagenfeldt; Juan Luis Cano; Luis F. Peñín; Claudio Bombardelli; Jesús Peláez; Eleonora Luraschi; Andres Galvez

This paper shows the GNC design process for a mission aiming to find, approach andmodify the orbit of a small asteroid. A large number of such bodies are orbiting the Sun in our Solar System, and some of them might become a real threat for the Earth during next few decades. While the size of the asteroid, besides its orbit, greatly determines the attention that should be given to any specific body, it is also necessary to start developing the concepts and technologies required to face these kind of challenges. For this purpose, these small asteroids represent a good training opportunity, since they allow testing the intended orbit modification principles with reasonable mission/system needs and with no impact risk for the Earth.


7th International Energy Conversion Engineering Conference | 2009

Electrodynamic Tether for Scientific Mission at Low Jovian Orbit

Juan R. Sanmartin; Mario Charro; Claudio Bombardelli; Enrico Lorenzini

An electrodynamic bare tether is shown to allow carrying out scientific observations very close to Jupiter, for exploration of its surface and subsurface, and ionospheric and atmospheric in-situ measurements. Starting at a circular equatorial orbit of radius about 1.3/1.4 times the Jovian radius, continuous propellantless Lorentz drag on a thin-tape tether in the 1-5 km length range would make a spacecraft many times as heavy as the tape slowly spiral in, over a period of many months, while generating power at a load plugged in the tether circuit for powering instruments in science data acquisition and transmission. Lying under the Jovian radiation belts, the tape would avoid the most severe problem facing tethers in Jupiter, which are capable of producing both power and propulsion but, operating slowly, could otherwise accumulate too high a radiation dose . The tether would be made to spin in its orbit to keep taut; how to balance the Lorentz torque is discussed. Constraints on heating and bowing are also discussed, comparing conditions for prograde versus retrograde orbits. The system adapts well to the moderate changes in plasma density and motional electric field through the limited radial range in their steep gradients near Jupiter.


Astrophysics and Space Science | 2006

Far-Infrared/Submillimeter Astronomical Interferometry with Spaceborne Tether Formations

Enrico C. Lorenzini; Claudio Bombardelli; Mario L. Cosmo; Martin Harwit; David T. Leisawitz; Rodger Farley; Stephen A. Rinehart; David A. Quinn; David W. Miller


Advances in the Astronautical Sciences | 22nd AAS/AIAA Space Flight Mechanics Meeting | 29/01/2012 - 02/02/2012 | Charleston, South Carolina, USA | 2012

Relative Dynamics and Control of an Ion Beam Shepherd Satellite

Claudio Bombardelli; Hodei Urrutxua; Mario Merino Martínez; Eduardo Ahedo Galilea; Jesús Peláez Álvarez


Archive | 2001

Pointing Dynamics of Tethered-Controlled Formation Flying for Space Interferometry

Claudio Bombardelli; Enrico Lorenzini; Marco B. Quadrelli


SPACEFLIGHT MECHANICS 2012, ADVANCES IN THE ASTRONAUTICAL SCIENCES | 22nd AAS/AIAA Space Flight Mechanics Meeting | 29/01/2012 - 02/02/2012 | Charleston, South Carolina, USA | 2012

The SIROCO Asteroid Deflection Demonstrator

Claudio Bombardelli; Hodei Urrutxua; Andres Galvez; Ian Carnelli


Advances in Space Research | 2011

General Relativity Accuracy Test (GReAT): New configuration for the differential accelerometer

Valerio Iafolla; David M. Lucchesi; Sergio Nozzoli; M. Ravenna; Francesco Santoli; I. I. Shapiro; Enrico C. Lorenzini; Mario L. Cosmo; Claudio Bombardelli; Joshua Ashenberg; P. N. Cheimets; S.L. Glashow


Archive | 2008

A Kilometer-Baseline Far-Infrared/Submillimeter Interferometer in Space

Robert Smythe; Harold W. Yorke; Enrico Lorenzini; Claudio Bombardelli; Ronald J. Allen; Daniela Calzetti; Andrew W. Blain; William Doggett; Antoine Labeyrie; David A. Neufeld; Shobita Satyapal; Gordon J. Stacey; Edward L. Wright; Nicholas M. Elias; David Fischer; James Leitch; Tracey Espero; Lockheed Martin; Charles F. Lillie; Northrop Grumman

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Enrico Lorenzini

Smithsonian Astrophysical Observatory

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Ronald J. Allen

Space Telescope Science Institute

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Daniela Calzetti

Space Telescope Science Institute

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David T. Leisawitz

Goddard Space Flight Center

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