Related & Interesting Projects
Here we list related and interesting projects.
Cosmic Hot Interstellar Plasma Spectrometer (CHIPS)
During the Goldin era there was a push for UNEX (University Explorers)
and the results was the 63-kg
CHIPSAT. This satellite was launched on January 12, 2003 and
was turned off (due to budgetary reasons) in 2008.
The papers by Janicki (2003) and Taylor (2003) give a perspective of
CHIPSat from the design team (SpaceDev) and that by Sholl (2008) gives a
nice summary of the lessons learnt from the mission. The principal results
of CHIPSat are two papers: Hurwitz et al. (2005) and Sasseen et al. (2006).
Literature on ChipSAT
-
Opto-mechanical Design of the
Cosmic Hot Interstellar Plasma Spectrometer (CHIPS)
by M. Sholl et al. (2003) [SPIE 4854, pp. 467]
-
Optics design and performance of the
Cosmic Hot Interstellar Plasma Spectrometer (CHIPS)
by M. Sholl et al. (2003) [SPIE 5164, 63-73]
-
The CHIPSat Spacecraft Design -- Significant Science on a Low Budget
by J. Janicki and J. Wolff (2003), [SPIE]
-
CHIPS: A NASA UNEX mission
by E. Taylor et al. (2003) [SPIE]
-
CHIPS Microsatellite Optical System:
Lessons Learned
by M. Sholl et al. (2008), [SPIE 7071, pp. 707104]
-
Observations of Diffuse EUV emission with
CHIPS by Hurwitz, Sasseen and Sirk (2005) [ApJ 623, 911-916]
-
A Search fo EUV emission from Comets with CHIPS
by T. Sasseen et al. (2006), [ApJ 6650, 461-469]
The Project Manager (Sholl) is at SSL, UC Berkeley and the Project
Scientist M. Hurwitz is now a teacher in Bay Area.
Microvariability & Oscillations of Stars
The
MOST is Canada's first
astronomical satellite.
Need a volunteer to summarize this mission.
BRITE
BRITE-Constellation
is a cluster of "nano-satellites" each costing $1M and aimed
at high precision two-color photometry of the brightest stars in
the sky (less than 4 mag). The science payload is 30-mm f/2.3 lens
coupled to an interline CCD (35-mm format). The FOV is 24 degrees.
BRITE Austria effort
encompases several Universities in Austria and Canada aims at
building a line of "nano-satellites" (less than 10 kg). The
statements from their Mission page should resonate with our dream:
"The [TUGSAT-1] satellite makes use of recent advances in miniaturised
attitude determination and control systems" and "A major goal is
sustainability. TU Graz plans to develop a generic satellite platform
which can be used for future low-cost space missions for which
interest by the scientific community and industry exists."
Each satellite is equipped with UHF antennas, a slotted S-band
antenna, magnetometer, GPS antenna, star tracker and solar
panels. The satellite volume is 20 x 20 x 20 cm^3 and
the total mass is 6 kg. Attitude determination is provided by
the magnetometer. Three reaction wheels and corresponding
magnetorquer coils provide for three-axis attitude control
and momentum dumping. The attitude control accuracy
is better than a degree, attitude stability is one arcminute
and attitude determination is 10 arcseconds. Ground stations
are modest telescopes at Montreal and Graz.
Monitor e Imageador de Raois-X (MIRAX)
MIRAX is a project of the Brazilian Space agency (and the only
known astronomy project). MIRAX aims to observe the Galactic center
and bulge regions in the energy range, 2--200 keV (essentially using
two sets of coded aperture masks instruments). The total mass is
200 kg and the consumption is 240 W. The estimated cost is pegged
at $10M. It seems to be under development since 2002. Please
find a presentation and a paper.
Jump to
the top