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:���A8�X�r ���^%ʣ֛������C��/��� �6[#�5#��:��U����U�{�����A��[�X���� s���hxd�/=���.�ݟ��Y���S�;(���׿)6�'8���')�d� =��s�#:�#U�l�Yu:=�0���*wQ]�����0�����g%��������^[8.��:U�WO�+Tִ�72]HN�OU�[�KhX����k>U�o5�@m�b���r��؆���η��U����z>� ��f1�����O����R���߬a/'���b�Ⱔj�-,`�ǻhF High Performance. ��Jf�������^�x���]߿|!����E) 2 0 obj �g��3A�9��x�\`��~V����&����7��L���R`�澵Gq��� P�\�F����\�R#�b5���G�I���Th�@�@���]Z ^C�K�cv����^� ^�$S#��k�~`Wѫ��b�$|��V=\ A�^ZL2x.e���j�2�Ƚ �贖Z ��DA�8 �,����"��ꒆ�A��c���b�2AE~�e3�Yͥ��*��,�T^��%fGŐ�� nD1XW�E0Pd�����D1\����C��fq�}%^c)�F�2A�wY�]��\W��;���$���VbfSG7+H�ŭ�*�nB)B`N�I;�e�E/��V�Pu&�`��OU����`�Q���7M����N��18�K�^҅��4XX�.�Q��:ꫫ�|Q��������%Og 38�k/n1s �L��˽��i2�u�`��0f�S\���/VS%" H�P�u��2�ʙ���������0���݊�f���/�,�#�618��Kbc�ۢ�����l�p��CN�B]�(q�ؖ���2�11b;H��Ia{+iو�rq�Ǔd�n[Y̤��!��1�txƘR$_�P����sĀE�X���S`s(Ƒ��:8aLU��"��ɣ� ��#�g��D�3��Y�N�fcDrY$ {��To%��(���{o�O�����R�����Qhhc�9-��|�`��@�E��n�"��6J��dSi'�7�!���Q���˩B���[�OH��:� �"j��O@ϰ8��x ���,�. <> No more than two emails per month, you can unsubscribe any time. stream <> 7 0 obj �� � w !1AQaq"2�B���� #3R�br� A spacecraft bus for a high performance 12U CubeSat. x��]�s�8�OU�>J[g��"��)�M2�ݹ��d���Ue�A�i[Y��R��_� J�L�M���}�#~��F����n��q�]\������7ٿ^�(�"/�B8%DV <> The supported ISIS ‘standard’ CubeSat sizes and envelopes for both its CubeSat Structures product line and its CubeSat deployer product line are outlined below. 1U 1.5U 2U 3U 6U 6U-XL 8U 12U 12U-XL 16U ISIPOD DuoPack QuadPack 12U ���� JFIF ` ` �� C �� C CubeSats no longer have to settle for sub-optimal orbits or short duration missions. I would like to receive an up-to-date information about NanoAvionics products and industry news. ݺ=9Z��1VSA(gi��T5�9��|�U'P� 1 0 obj endobj �r�$�!kEFJw��"UTqr̸�KQ�N@���Ngr��T`b�2�<7�ɡ�R�>�p�o�w����If�s�A*+�f.F��k}��ԅʵ|� ��fQsS�**5��6�/�K���b�J���R��hb���y��[�

�?�<=k�2׾ =�x��쏩�M!IR. Very soon 16U from US or 20U from China. 12U CubeSat is 20 cm × 20 cm × 34.05 cm.

<> 2 CUBESAT BUS INTERFACE DEFINITION A standardized backplane (BP+FAB) implements the entire harnessing. The system is designed to save customers’ time and budget, minimize required integration effort and effectively increase volume for payload as well as overall system reliability through matched hardware on one board. 10 0 obj 1U CubeSat is 10 cm × 10 cm × 11.35 cm.

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stream F��V�ȫ2z��y�z�š�. ��8�(�HTGx��*��;��P�i CubeSat 101: Basic Concepts and Processes for First-Time CubeSat Developers NASA CubeSat Launch Initiative Produced under contract by the California Polytechnic State University, San Luis Obispo (Cal Poly) CubeSat Systems Engineer Lab The same M7-core MCU performs OBC and ADCS functions. $4�%�&'()*56789:CDEFGHIJSTUVWXYZcdefghijstuvwxyz�������������������������������������������������������������������������� ? endobj endobj <>/XObject<>/ProcSet[/PDF/Text/ImageB/ImageC/ImageI] >>/MediaBox[ 0 0 595.2 841.92] /Contents 4 0 R/StructParents 0>> 2U CubeSat is 10 cm × 10 cm × 22.70 cm. endobj Commercial missions require spacecraft busses suitable for longer mission time that can accommodate bulky payload. endobj 3 0 obj <> 9 0 obj Smallest launched CubeSat is 0.25U and largest is 12U as of 2019 January. eN����{�"{o}��F�[�-�:��\����y��c��!%+l���ܷ��\�f������+m�Z�e��g?���ݛ_~ʊ����O�Iz���"����O?��B}�¾��2����FgJ䅁+�M/B���O� �ۥ���O+���d��勷ð�pXJ�\�P�O�3�}9F�X ���1h�h�D.�I= Gj�B���t�г�ʼ�W�r���q�WfҖ���V03� �� *�" ��

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SatBus 3C2 is a highly integrated nano-satellite main bus unit containing advanced functionality: SatBus 3C2 is a flight computer tailored for small-sized satellites and complies with the CubeSat standard. OYUdB���\�Cť*4�"C�?z���$5����%G���AS�r������a2)%G�Qg��bf��_jt*��tt8��&�%�n��c��3�w*$��D��6UU������zX�Ǿ�N~3�� O��z�-����R0]"� �Y9c��-f��5��u��n){HU��f�/����wS5�,j��!�!Y[�hg҆y�j�hN*{H�6�r�C����p�cS�_No,{��6$S�+H"x������C�*ae E�CN�sa~8���[͉/�N�N�����B��\KKg�koל��!��(�Wq�a9�F��j*̄]q,{�6�JҒ�sL�h��Y��Cb�Yb�G\,a��^/�A�Cp�A�mQ@����7���_^����H�����f5���P�X�Ԯb0~�s��}�g�X��S������@h��rx��Ķ���{;�e[����=��Fn{j�CG�,�C���s=�.���V������O)��C2�}�Ѽ2F�Gg;l��v�������n����(�#dx �W���(����tC��Q�3��Ek����'�׿�َ���;�P�*��E� ޲w�=�am�=a�ㄖ�����Gß�X[� ^��pqC�W�o��,U�

Subsystem boards and satellite side panels can be plugged to the backplanes subsystem bus interface and panel bus interface, whereas the panel bus represents a subset of the subsystem bus. At NanoAvionics we are always looking for talented people to join our professional team. <> endobj x��TMk�0���hv,i4����~�li m��zpﲐح����w�7UW6$F��{< T�puU�,�Kէ��CѴ��w��5̗�o�z/�lvy&A�_�t�U���c� d�A�*�N���~��g��m�����u=��w�|̳U��^H���5�}�Fj�d�4��X�"T>^���+gd̙?v�E"0&4�G��C�=�匊�6-�X�ñ4š��� �y�8�.9GB�p��"r��CX�RX��1H����_v�'Z�O�҈T(L�4'�LO�YZ����Nd�e�衴�Oiݤ"2�Q)�6Q9����R�B��}"� oY\�! ��^.[�$jP���T�t�c�. 3 0 obj ����V,[.V������J��c�Vg̓�Ė�����7�\l�4�c�[o��l�$.�F��Je>F���穙���&��I1��� �O���M�����x��̦j���j���+xJ�����Vt �SB��lߕ:8�Zs�_�\V�� Y��e��(�c'P�65{�6����S�K腇�j��� SatBus 3C2 architecture is based on an STM32 H7 series microcontroller with high-performance and low power ARM Cortex™ M7 32-bit core MCU, operating at a frequency of up to 400 MHz.

NanoAvionics is offering a developed and in-orbit tested satellite operations system – Main Bus Unit “SatBus 3C2” with ADCS, including necessary sensors and actuators. <> endobj endobj <>/Font<>/XObject<>/ProcSet[/PDF/Text/ImageB/ImageC/ImageI] >>/MediaBox[ 0 0 612 792] /Contents 4 0 R/Group<>/Tabs/S/StructParents 0>> endobj %PDF-1.4

��h�4DV����H�G�ӄlz2�r�I� ;n�Pa���$��D�7b�P�*�G���\�C�)-��X�� Standard 12U bus Revolutionary 12U Solar Electric Propulsion Module ExoTerra’s revolutionary 12U Solar Electric Propulsion Module, Courier, brings large satellite power and propulsion performance to the CubeSat world. %���� <> The use of CubeSats for commercial purposes is ever-increasing. �[���vw]�h��.g�+��T��L}f&�����3�$+�N��4���?�#�֠].���K�o_;q���p�D�4�+ :��׾�!bd��g3���Y��|���Q�h��M�}{m�i"��D��D��4j>�2lq�~����������.�7j 8 0 obj A number of various digital interfaces are available for sensor and other CubeSat hardware support. Dispenser rails extend the entire length of the satellite, however, CubeSat rails may be discontinuous between the CubeSat standoffs, with at least 75% of aggregated rail length being … endobj stream <> NanoAvionics CubeSat On-Board Computer - Main Bus Unit SatBus 3C2 is a highly integrated nanosatellite flight computer containing advanced functionality such us an on-board flight computer (OBC), an attitude determination & control system (ADCS) and …

Smallest existing CubeSat design is 0.25U and largest is 27U. I understand, that NanoAvionics can store and analyse data entered in this form in along with my browsing activities in order to fulfill my request and/or provide an improved user experience, An attitude determination & control system (ADCS), Redundant UHF communication system (COMM), Dual (Redundant) UHF Digital Radios “SAT2RF1-1D” onboard, Cortex-M7 core, clock speed up to 400 MHz (configurable), 200 MHz typical, 256 MB of external NOR-FLASH for data storage (2 × two die (64 MB each) chips, QSPI), 2×512 kB of FRAM (SPI) for frequently changing data storage, On-board magnetometer and three gyroscopes, Multiple CAN, SPI, I2C, UART/USART interfaces. CubeSat Buses and Architectures Dellingr-X: GSFC’s solution to enable planetary science missions Colby Goodloe colby.s.goodloe@nasa.gov 301-286-2444 Mike Johnson, Larry Kepko, Chuck Clagett, Luis Santos, Tom Johnson Courier’s550-800 m/s ∆Voffers the <>/OutputIntents[<>] /Metadata 921 0 R>> %���� SatCOM UHF (1 pcs) Sun sensors (6 units) Reaction Wheels 4RW0 (1 set) Magnetorquers (1 set) GPS Receiver (1 set), Fill in the form to access M6P technical summary, CubeSat On-Board Computer – Main Bus Unit SatBus 3C2, Submit your e-mail for our news and announcements. x�D���^K ��Q�0�j)p�����A��E���s���n�c�r+�u�A��\�V���&�����c�O����JҿPԘ& �g�@����`hEv��b�,*$�88}�9��ջz;�����ߎ�1��9��O� ��.w�u�4��K"���m�"��$�ط�3�4}�@O"�! ��W4�)Ojr��S�^�&���c�ړ� C�zOŒ�� %&'()*456789:CDEFGHIJSTUVWXYZcdefghijstuvwxyz��������������������������������������������������������������������������� The resulting electrical structure is 11 0 obj <>/Metadata 652 0 R/ViewerPreferences 653 0 R>> �� � } !1AQa"q2���#B��R��$3br� endstream %PDF-1.7 ̧�2Οڅ1�(�Q�vՏ�P�j��c�gBKN���u?���B�P,9C%���FQ�����4Q�ū(H]c�������I�F�,m�̝���d�,Y�{����9T�*+�P� 3{��j�''��`Q+t�t���[��Pל�[S�bQ:�&�L�:���j+H���. Orbital Transports has a variety of satellite bus and platform options to help facilitate your cubesat mission in our SmallSat Catalog. 2 0 obj

��k��瀤�dO��X����q�����Sm�}����]s@R��S {�k�nk�+�*B%������� The 12U dispenser includes four rails that cradle the satellite on all four corners. 6 0 obj 4 0 obj endobj Sounds like you? 6U CubeSat is 20 cm × 10 cm × 34.05 cm. <> endobj

4 0 obj External flash and F-RAM memories provide reliable storage for telemetry and user data.

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