Student Launch Project
Download
1 / 35

Student Launch Project Flight Readiness Review April 21, 2014 - PowerPoint PPT Presentation


  • 137 Views
  • Uploaded on
  • Presentation posted in: General

Student Launch Project Flight Readiness Review April 21, 2014. Team Structure. Presentation Overview. Final Launch Vehicle Final Motor Selection Static Stability/ Mass Margin Recovery System Full Scale Test Flight Verifications Integrated Research Payload.

loader
I am the owner, or an agent authorized to act on behalf of the owner, of the copyrighted work described.
capcha

Download Presentation

Student Launch Project Flight Readiness Review April 21, 2014

An Image/Link below is provided (as is) to download presentation

Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author.While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server.


- - - - - - - - - - - - - - - - - - - - - - - - - - E N D - - - - - - - - - - - - - - - - - - - - - - - - - -

Presentation Transcript


Student launch project flight readiness review april 21 2014

Student Launch Project

Flight Readiness Review

April 21, 2014



Presentation overview
Presentation Overview

  • Final Launch Vehicle

  • Final Motor Selection

  • Static Stability/ Mass Margin

  • Recovery System

  • Full Scale Test Flight

  • Verifications

  • Integrated Research Payload



Key design features
Key Design Features

  • Launch Vehicle Sections

    • CubeSat, Hazard Detection, Multi-Staging

  • Fin Style

  • Launch Vehicle Separations

    • Booster Section, Drogue Bay/ Detachable Bulkhead


Forward section cubesat
Forward Section - CubeSat

  • Nose Cone

  • Voltmeter

  • CubeSat


Avionics payload section hazard detection
Avionics/Payload Section - Hazard Detection

  • Avionics/ Payload components

  • Hazard Detection System

  • Drogue bay disengagement


Booster sustainer section multi staging
Booster/Sustainer Section - Multi-Staging

  • Booster section disengagement

  • Fin Style and attachment

  • Positive Motor Retention










Predicted drift from launch pad
Predicted Drift from Launch Pad

Predicted Altitude








Key design features of the payload
Key Design Features of the Payload

  • Hazard Detection System

  • Lateral Vibrations In line System (LVIS)

  • Tesseract


Payload design and dimensions
Payload Design and Dimensions

Hazard Detection/Avionics Bay



Payload design and dimensions2
Payload Design and Dimensions

Tesseract

  • Designed to measure the magnitude of accumulated triboelectric charge on the surface of the nose cone at carious altitudes

  • Time stamp all altitudes and charge measurements to assist in post flight analysis


Tesseract payload overview
Tesseract Payload Overview

  • The system can be broken down into three separate subsystems:

    • Voltmeter

    • CubeSat

    • Ground Station

  • The nose cone will be coated with MGM Chemicals 838 Total Ground Carbon Conductive Coating


Payload integration hazard detection avionics bay
Payload IntegrationHazard Detection/Avionics Bay


Payload integration lvis
Payload IntegrationLVIS

  • Locations of Raven3

    • Avionics Bay

    • Above the Sustainer

    • Mini-Avionics Bay

Raven3 on payload sled

Raven3 diagram from manufacturer’s website


Payload integration lvis1
Payload IntegrationLVIS

  • Electrical schematic of RockeTiltometer2 with Raven3

Image of RockeTiltometer2 with connections


Payload integration tesseract
Payload IntegrationTesseract

1

2

6

5

4

3


Interfaces with ground systems
Interfaces with Ground Systems

  • Internal Interfaces

    • Nose cone and payload sections

      • All-threads

      • Bulkhead-like centering rings

      • Nut locks

    • Drogue bay, avionics bay, main bay, sustainer section, booster section and mini parachute bay.

      • #2-56 nylon shear pins (x3 for each section)

  • External Interfaces

    • 1515 rail buttons

    • Parallel booster attachment points




ad
  • Login