The+Jig+v2.0

=The Jig v2.0=

This page will contain reports on the design progress of the second MARS testing rocket, The Jig v2.0. It should be clear and concise, with each design team responsible for keeping their own section updated. Any drafted part files should be added to the section at the end so they are all together, sketchs and images may be placed in line.

Here is a list of fixed parameters, all designs should be made with these in mind. Any changes to these values must be justified and discussed with the MARS President (Nicholas Tegg), he is the only one who may edit them.
 * Global Parameters**

-63.5mm diameter inner tube -all screws used are m6 -combustion pressure is 375psi -all pipe thread are bspt 1/4 inch. See here for standards. -assume graphite nozzel -material of structure is aluminium (try to choose a common type please) -length is unknown and will be determined later (its not important to performance) -design everything with weight more important than thrust

IMPORTANT **All stock pressure values are given to us in PSI, but all our design work must give both PSI AND KPA (**1 //psi// = 6.8948 //KPa//**).** **All stock pipe values are given in INCHES, but all our design work must be in MM (**1 in = 25.4 mm**).**