The Rocket Team runs a program each year to help new members design and build an L1 cert rocket. As part of the program, members use OpenRocket to design a rocket from a set of standard parts. These parts are then ordered in bulk and distributed in custom-made 'kits'. Team members then assemble their rockets from these parts in supervised work sessions, and launch together at a public launch somewhere in New England (CATO, RIMRA, and CMASS organize launches regularly). 

Part List

We use Apogee parts to assemble the L1 'kit'. The following parts are required for each student:

PartDetailsOrder Link (correct as of 28 Nov 2020)
Body TubeLOC BT3.00 - Cardboardhttps://www.apogeerockets.com/Building_Supplies/Body_Tubes/High_Power_Tubes/3-00in_LOC_Body_Tube
Nose ConePNC-#.00 (75mm) for Thick Wall Tubeshttps://www.apogeerockets.com/Building_Supplies/Nose_Cones/High_Power_Nose_Cones/PNC-3-00_75mm_Thick_Wall_Tubes
Motor Mount (Inner) Tube29mm Thick Wall Cardboard Tube - Cut to lengthhttps://www.apogeerockets.com/Building_Supplies/Body_Tubes/29mm_to_54mm_Tubes/29mm_x_34in_Thick_Wall_Tube
Shock Cord1500# Kevlar Cord - Need ~2 body tube lengths per rockethttps://www.apogeerockets.com/Building_Supplies/Parachutes_Recovery_Equipment/Shock_Cord/Kevlar_Cord_1500
FinsCut from 1/8" Plywood - Custom shape 
Centering RingsCut from 1/8" Plywood 
Rail ButtonsStandard Rail Buttons - may need different screwshttps://www.apogeerockets.com/Building_Supplies/Rail_Buttons/1in_1010_Rail_Button_Standard
Motor Retention Clips2 Screws w' Washers work well 

In addition, the following parts are owned by the team and shared

  • 29mm 3 & 4 grain motor cases
  • Parachutes
  • Nomex Parachute Protectors
  • Igniter sets

We recommend Cesaroni 29mm H (I is ok as well) motors (e.g.H87) - these can be bought from Apogee or on-site at some fields

Design Criteria

After students submit designs in OpenRocket, they should be evaluated based on the following criteria before ordering parts:

  • The correct parts are used (unless the student plans on buying their own parts)
  • The simulated altitude is below the waiver limit for the planned launch field
  • The stability off the launch rail is acceptable (~1-2.5 calibers) for the following cases
    • Ideal launch conditions (4 mph winds, no launch rod angle)
    • Worst-case conditions (9 mph wings, 3 degree launch rod angle)
  • An appropriate delay for the flight has been selected
  • The fins have tabs that are connected to the inner tube (through the wall construction)

Design Presentations

Presentations can be found on the parent page

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