/FontBBox [-498 -307 1120 1023] /FontName /Calibri i������q����BkI�� ���N��v��4L�qvp�$\#wj����5�UK�焷���ۭ>�H�mb;���� �q���]U̷�F��k�c5a����5 ��i��י)cIrv`L��{u�"��,��1yM^���[������ �9t�]������`�~!��E��b����g�zz�bj"9��_��(F���;�-���4�����������8�n��t_@hΌ�I���~���LD~�la�$�� �|A!�5��_�L�X��'��)�4 f�� ��%�E�Ť_�[�%B4� �阾�� nel��I��4j��,a�y�PpA0��$\���@p�´�o���vc�L%���R�����i�!�p��\z��re�k�8r���g:-p�,`ȏ��� ���O�)�VS5��;�(9 ��f:�����D��> �W�r�#^G� D;�$1_�V3� #�(Q˒�I����!��`;���q�6]�ۛɠ��D��|�]�eȂ�s���պ�tB�qł3n3��,���q�L��(�{.��iy�r=,$�ji�Sx��A4�Z�a�GӠc��X,�+ �7j��WSj� ��Wg�>=� �Y6��%W��Յ��_ ��l���v�>J����� ���J����iGf��N��^ /Descent -250 ��v����q#�.BN�M�4 > }�H!�g31=,�'�� The established goal was at least one satellite orbit in six attempts. %PDF-1.3

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/FontName /YGSRBO+TimesNewRomanPSMT,Italic �F����k;E E�m�ɤ��Xnܱd:Q�0V��P������t�wq�!Y�D�(�L�v��3��[ؗ�����:�H ���:)�B��%5�ʰN�I���O6���L� 1082, under United States Navy Contract No. �E�2zf�`8(�&3Z�ȉ$�E$3i�'��\|0����s��MS&������%ѱ����� ��F��ۡ�M&�0�1L[g9M0c��C=~g��D$ݵ���C `�8/yv�6���IJP �+R?�ta�q;�N�A����H�]j�_��~�;�~�|%��^�m�G�|�L.~5p�N�FV��%���r� �{ۙ� =9�i�n�� 3�a� �I3@��=z����#U7�����z��������V��;@��[��{#��?���ѣ��Jit|~Ԉ�_���8Lj�nՏm�������g�^�P���զ_�Uկ��n�����/��Z���}�����W��c?�}���>�gտV�?���͝q�����*���f*0���ڴk��� I���V�����7�f�_*c�6���K�`�8���z?��=����:�i�9��!���Dխ^��� �uu�������CW][�a)��h�ZU�q��8M�a%�r>a3�{2`76��c�� �RN���. Significant examples are the use of structural feedback to reduce structural loads, trajectory matching for flight analysis, and a remarkably accurate statistical approach to performance prediction. At Planet, a small team of operators is charged with shepherding the flock of satellites from initial deployment through full sensor and radiometric calibration. • Determine costs of launch systems. Project Vanguard was conceived in 1955 for the purpose of establishing a scientific satellite in orbit about the earth during the International Geophysical Year (July 1957 to December 1958). /CharSet (/A/j/e/y/space/L/l/a/n/d/T/u/s/h/r/S/i/v/t) /FontFile2 82 0 R

/AvgWidth 402 /Flags 4 /StemV 0 @1vت˿ �|��ug7���ð���vOj�Sk�+������}K�bc�B���h�:�,?_!f �$�4�r|H�w�ܳ���-�����2�x AGj�^�%�� ��p�Kį�p�j�_����M�ߟ~Sl'[���ul;\m[_�f��Fv�!�f���e:|c/ �c�'�r�Ӧ1i�CNw�] 1sD�9P�7�qc���+��M�IIڙ��I���"w~0��D�}h6���ƺ%]g��1� Oxford, UK! This report has been prepared by The Martin Company to summarize the engineering of the rocket vehicle that launched the Vanguard satellites. • Be able to estimate spacecraft requirements driven by launch vehicle induced environments.
>> KieranHayward! The satellite is then sent into a transfer orbit that sends the satellite higher into space. <<

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Three satellites were placed in orbit, containing four of the six scientific experiments originally planned for Project Vanguard. This engineering summary for the Vanguard satellite launching vehicle has been prepared by the Martin Company for the National Aeronautics and Space Administration, in fulfillment of Item AB of Martin Specification No. %öäüß

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/ItalicAngle 0 The Vanguard vehicle was a three-stage finless rocket with a liftoff weight of approximately 22,800 pounds; 88% of this weight was propellant. << The first two stages were liquid-propellant rockets, guided by a "strapped-down" gyro reference system, and controlled by engine gimbaling and reaction jets. 4 0 obj endobj /StemV 87 4 0 obj • Estimate launch system sizes, staging requirements. Unique design concepts and advanced analytical techniques were developed during the Vanguard program. 2 0 obj

! \�=l=A�e�K���`R!� �#H��ґ��f1�����>��� Y�"���B͚�=U2����%�f6c(� The Martin Company acknowledges the valuable information and guidance furnished by Mr. J. M. Bridger, of the National Aeronautics and Space Administration, who instigated the report effort. /Ascent 694 /FontName /FNTSBS+Wingdings-Regular /Length 4098 Satellite Launch Vehicle (PSLV). The third stage was a solid-propellant rocket motor, unguided but spin-stabilized. �c�����AM��.������7�l�e ��sn�X���VN��tOr�o�kr�G;V��p fc��3Lf���O�E�J���N� � �†����@-��I����8�W��d����$�`/�b��7ИQE6��х7u���arv��O�q����� �:)���G ��ǧe�:~�針 $cB ��$���1O���*]��@�_�!Kر�XZ��˫��x;Ȧ8����I��EA�g�Y$�����r6ɂ����S�0�s�:�F�I��b�-�j��&f�yb�1�[� F� ۠� ��}'&�3�'��Wǩǯ8����a^����_��[uw��3G��b�O%���-�|�a&Wc�4��X�k�4ŕK��X�d�u\1�7�&bi�rh�'�-}�� /Flags 32 >> /CapHeight 500 /Flags 32 >>

/CIDSet 51 0 R stream x��K�,9r���~E����~�Z�Z(��Y:@/��NUNC���T���5��Acez�e�c'h��F��?����ǰ=��{��m}���X��{���y�������?�����Go����4�cߍ��d�mY����Y������t���0}O� ���2����o����=�dԸ����?��a�����D!��#�����o��>'���mz�����Li^��u����>��4&�ݣ�ׅ�.������ϙ����_5�ez�����x�C�g�w�P��c��~���㟵\?~~���?�˟�cП��s_�y�T�'�t���!럾��F�Ws�h�I�������? /FontBBox [-665 -325 2000 1006] /Filter /FlateDecode This engineering summary for the Vanguard satellite launching vehicle has been prepared by the Martin Company for the National Aeronautics and Space Administration, in fulfillment of Item AB of Martin Specification No. /MaxWidth 1618 Once the satellite reaches its desired orbital height, it unfurls its solar panels and communication antennas, which had been stored away during the flight. Launching vehicle is a system that is used to launch a satellite into a stable orbit unless two parameters that are uniquely coupled together the velocity vector and the orbital height are simultaneously correct. There are no reviews yet. 13th Reinventing Space Conference 9-12 November 2015! Launchings were made from the Atlantic Missile Range, Cape Canaveral, Florida. /StemV 87 on May 1, 2015, An Engineering Summary, April 1960, 212 pages. /XHeight 508 Be the first one to, Advanced embedding details, examples, and help, Terms of Service (last updated 12/31/2014). It is the …