Preliminary Design Review

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Presentation transcript:

Preliminary Design Review Presented by: RCS Engineering

Contents Team Summary (1 min) Revisions Made Since Proposal (1 min) Safety (2 min) Launch Vehicle (5 min) Payload (5 min) Budget (2 min) Educational Outreach (1 min) Questions

Team Summary Six team members Team Captain: Andrew 5 High school and 1 Middle school Team Captain: Andrew Safety Officer: Cristian Mentor: Tracy Burns NAR#998115R Cert Level 2

Revisions Made Since Proposal Changes to Launch Vehicle Overall Mass Motor Selection Changes to Payload New Objective Changes to Project Plan Budget Outreach

Safety Risk Assessment Hazard Identification Potential Consequences Preparation and Prevention Risk Assessment Efficiency

Launch Vehicle Specifications Motor: Aerotech K1103X-14 Total Weight: 13 pounds Thrust to Weight Ratio: 19:1 Stability Margin: 1.8 Calibers Max Velocity: 619 mph (Mach 0.82) Dual Deployment System Material: G12 Fiberglass Velocity off 120 inch Rail: 83 mph Total Length: 74.5 inches

Flight Profile

Recovery Subsystem Dual Deployment System Dual Redundant Stratologgers Black Powder Ejection Charges Ground Testing Planned

Payload Specifications Weather Data Collection Barometer and Thermometer Arduino Active Telemetry System 915 MHz From Apogee Received On Laptop

Budget Funding Plan BBQ Plate Sale Bake Sale Team Merchandise Grants Local Businesses Politicians

Educational Outreach Pre-K and K Outreach (Completed) Community Rocket Launch (Completed) UNA TARC (Ongoing) TARC Mentoring (Ongoing) UAH Propulsion Labs (Upcoming) Astronomy Night at Cypress Cove (Upcoming)

Questions?