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UTIAS/SFL provides a low-cost launch service for nanosatellites. This service was originally motivated by the needs of the Canadian Advanced Nanospace eXperiment (CanX) program. The CanX program demonstrated a need for reliable, low-cost access to space for regular (18 to 24 month)
launches of 1-5 kg spacecraft.
A principal feature of the approach taken by UTIAS/SFL is to mitigate
the technical and financial risk shared by the spacecraft developers who
are partners in a particular launch, while maintaining reasonable costs
and ensuring timely delivery. UTIAS/SFL continues to collaborate with
launch providers to address the needs of the nanosatellite community by
reducing the real cost of coordination incurred by launch providers and
spacecraft developers.
UTIAS/SFL arranged the launch of its first experimental nanosatellite,
CanX-1, along with two Danish nanosatellites. The three nanosatellites
were integrated into a CalPoly P-POD separation tube. The integrated
system was dubbed "Nanosatellite Launch System 1" or NLS-1. UTIAS/SFL
also arranged the launch of QuakeSat - an American satellite built for
the purpose of early earthquake detection. The second launch system,
NLS-2, consisted of QuakeSat and its own dedicated P-POD. Both NLS-1
and NLS-2 were successfully launched from the Plesetsk Cosmodrome in
northern Russia on 30 June 2003, via a Rockot launch vehicle. NLS-3
was integrated as part of the ESA SSETI-Express spacecraft, which was
launched on the Cosmos-3M in October 27, 2005. UTIAS/SFL has negotiated
the launch of NLS-4 which will include nanosatellites from Canada,
Denmark, Germany, Japan, and the Netherlands.
![[NLS-1 Satellites: AAU Cubesat, DTUsat, CanX-1 in the UTIAS/SFL Clean Room]](nls-1.jpg) | AAU Cubesat, DTUsat, CanX-1 in the UTIAS/SFL Clean Room |
Nanosatellite Launch System 1
Launch Date: June 30, 2003
Launch Vehicle: Rockot
Separation System: P-POD Launcher (USA)
Spacecraft Complement: AAU Cubesat (Denmark), DTUsat (Denmark), CanX-1 (Canada)
UTIAS/SFL played a leading role in arranging the launch and supporting
the launch integration effort for three satellites during the Eurockot
Multiple Orbit Mission campaign. The integrated launch tube, NLS-1, was
launched on June 30, 2003 from Plesetsk, Russia.
Nanosatellite Launch System 2
Launch Date: June 30, 2003
Launch Vehicle: Rockot
Separation System: P-POD Launcher (USA)
Spacecraft Complement: QuakeSat (USA)
UTIAS/SFL played a leading role in arranging the launch and supporting
the integration and the pre-launch servicing of QuakeSat during the
Eurockot Multiple Orbit Mission campaign. The second integrated launch
tube, NLS-2, was also launched on June 30, 2003 from Plesetsk, Russia.
![[NLS-3: University of Tokyo students load XI-V into a UTIAS/SFL T-POD 1.7 in SSETI Express]](nls-3-loading.jpg) | University of Tokyo students load XI-V into a UTIAS/SFL T-POD 1.7 mounted in SSETI-Express |
Nanosatellite Launch System 3
Launch Date: October 27, 2005
Launch Vehicle / Parent Spacecraft: Cosmos-3M, ESA SSETI Express
Separation System: T-POD 1.7 (Canada & Japan)
Spacecraft Complement: NCUBE-2 (Norway), UWE-1 (Germany), XI-V (Japan)
UTIAS/SFL supported the integration of three nanosatellites with the SSETI-Express
microsatellite launched in 2005. UTIAS/SFL has developed three T-POD 1.7
separation systems for this purpose in collaboration with the University
of Tokyo Intelligent Space Systems Laboratory (ISSL) in Japan.
Nanosatellite Launch System 4
Launch Date: June 30, 2007
Launch Vehicle: Antrix Polar Satellite Launch Vehicle (PLSV)
Separation System: XPOD (5), Cute Separation System (1)
Spacecraft Complement: CanX-2 (Canada), AAUsat-2 (Denmark), Cute-1.7+APD II (Japan), COMPASS-1 (Germany), Delfi-C3 (Netherlands), SEEDS (Japan)
UTIAS/SFL has negotiated with Antrix for a June 30, 2007 launch of
six nanosatellites. UTIAS/SFL will lead the final integration and
launch campaign for the NLS-4 payload package. NLS-4 will use five XPOD
separation systems, which is an evolution from the T-POD 1.7 design used
in 2005. Three different sizes of XPODs will be used to accommodate the
different sizes of payloads.
Nanosatellite Launch System 5/6
Launch Date: late-2008 / early-2009
Launch Vehicle: TBD
Separation System: XPOD-II
Spacecraft Complement: BRiTE Constellation (CanX-3A, 3B, Austria, 3C, 3D, Canada), CanX-4 and CanX-5 (Canada)
UTIAS/SFL is planning to launch 4 to 6 nanosatellites in late 2008 and welcomes additional partners wishing to share the launch. XPOD and XPOD-II systems will be used.
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