1. Space Camp/Academy Huntsville, AL 2010

2. S.T.S. – The Space Shuttle –Orbiters –Space Shuttle Main Engines –External Tank –Solid Rocket Boosters

3. Launch Systems SRB’s SSME’s ET

4. S.R.B.’s – Height: 149 feet 45.4 meters – Diameter: 12 feet 3.7 meters – Weight: 1.3 million pounds 590,000 kilograms – Thrust: 3.3 million pounds 14.7 million newtons or 1.5 million kilograms Shipped to and from Utah via train!

5. Propellant: –Aluminum Powder (Fuel) –Ammonium Perchlorate (Oxidizer) –Iron Oxide (Catalyst) –Polymer Binder Double Batch Density of a pencil eraser 11 point star BEFORE AFTER

6. S.S.M.E.’s – Propellants: Fuel: Liquid Hydrogen Oxidizer: Liquid Oxygen Pumped from the External Tank – Thrust: 423,000 pounds 192,000 kilograms or 1.9 million newtons – Lifespan of 7.5 hours

7. E.T. –Made from aluminum –Pressurized when full –Coated in insulating foam –NASA’s giant soda can! –Fresh from the Bayou!

8. LH2 Tank – Liquid Hydrogen – -423 F / -217 C Intertank – Structural LOX Tank – Liquid Oxygen – -297 F / -147 C Three different components:

9. !! Demo Time !!

10. Launch!

11. Launch Timeline T - 6 seconds T 0 T + 10 sec T + 1 min T + 2 min ~T + 8 min 40 sec

12. Launch Timeline T - 15 seconds: Sound suppression T - 6 seconds: SSME start T 0: SRB ignition T + 10 sec: Roll maneuver T + 1 min: Max-Q (throttle back) T + 1 min 15 seconds: Max-Q over (throttle up) T + 2 min: SRB separation ~T + 8 min 40 sec: MECO ~T + 8 min 50 sec: ET separation

13. On-Orbit Orbiter OMS RCS Fuel Cells Payload Bay Crew Compartment ECLSS

14. Weight: 153,000 lb / 69,400 kg Height: 57 feet / 17.4 meters Length: 122 feet / 37.2 meters Width: 78 feet / 23.8 meters

15. O.M.S. (ohm-z) – Two OMS Engines – Use Hypergolic Fuels Fuel: Monomethyl Hydrazine Oxidizer: Nitrogen Tetroxide

16. R.C.S. – 44 thrusters on the nose and tail of the Orbiter – Same propellants as OMS

17. Demo Time

18. Three Fuel Cells provide electricity for the orbiter – Oxygen + Hydrogen = Electricity Water

19. Length: –60 feet –18.3 meters Width: –17 feet –5.2 meters Depth: –13 feet –4 meters Hitch a ride? –Not pressurized or temperature controlled Uses: –EVA and Cargo

20. Remote Manipulator System –RMS or “Canadarm” moves payloads and assists with EVA Orbital Inspection Boom –OIB is used with RMS to inspect heat- tiles for damage

21. The only pressurized and temperature controlled part of the Orbiter Equipment Bay Flight Deck Middeck

22. E.C.L.S.S. (ee-kliss) – Removes CO 2 – Cools avionics and equipment LiOH (lee-oh) Canister Active Thermal Control System

23. Demo Time

24. Landing

25. Review: Nominal Profile