Review of the Space Shuttle Program

Similar documents
Bob Hawkins Deputy Lead Engineer SLS Integrated Avionics and Software

Successful Return to Flight of the H-IIA Launch Vehicle

1.0 SCOPE AND INTRODUCTION. 1.1 Scope. 1.2 Introduction. 1.3 A Brief Description of the

PERFORMANCE AND TECHNOLOGY

Planned Orbital Flight Test of a 6m HIAD

Swiss Space Systems (S3)

Missions, Operations & Ground Infrastructure

PUZZLES CONNECT-THE-DOTS. A Collection of. of Famous Aircraft

WE BRING YOU THE LUXURY OF ROOM TO SPARE. MAKE OF IT WHAT YOU WILL.

By providing more capacity than any other twin-engine freighter, the 777F brings new levels of efficiency to the long-haul market.

Performance. Aircraft System

National Association of Rocketry Level 3 High Power Certification Requirements

CBO-750 ASSEMBLY INSTRUCTIONS

Capacity kw. Thermal turndown from specified maximum capacity 8:1 8:1

PERFORMANCE AND TECHNOLOGY

Launching a Sub-Orbital Spacecraft

Daher marks an aviation milestone with its rollout of the 800 th TBM aircraft

Rethink Convention. LINEAGE 1000E

ROYAL CANADIAN AIR CADETS PROFICIENCY LEVEL ONE INSTRUCTIONAL GUIDE SECTION 1 EO C WATCH HOW IT S MADE SEGMENTS PREPARATION

SpaceX rocket destroyed on way to space station, cargo lost (Update) 28 June 2015, bymarcia Dunn

The Boeing Next-Generation 737 Family Productive, Progressive, Flexible, Familiar

SPACE SHUTTLE MISSION SUMMARY INTRODUCTION

TWO SISTERSHIPS BEECHCRAFT 1900D. Available for Sale

Introduction to Aerospace Engineering

EQUATORIAL LAUNCH AUSTRALIA

EMBRAER PHENOM 300 SN RANGE (NM) 1,971 PASSENGERS 7 MACH 0.78 CONTACT: GREG OSWALD I

Forward Galley with Crew Rest Configuration Total Time Since New: 3,645.7 Hours

CALL INCREDIBLE ADVENTURES TO SCHEDULE YOUR TRAINING TODAY! CALL: 1 (800) / +1 (941)

Change> Deutsch Espanol Nederlands Português Svenska Française Italiano Россию International-English 中文

Arianespace Launch Service Operator Policy for Space Safety

ROYAL CANADIAN AIR CADETS PROFICIENCY LEVEL ONE INSTRUCTIONAL GUIDE SECTION 6 EO C IDENTIFY INTERNATIONAL AIRCRAFT PREPARATION

Valley Fliers 1402 Auburn Way North, #223 Auburn WA 98002

TUESDAY, NOVEMBER 11 COUNTDOWN STATUS BRIEFING KSC 9:00 AM 10:00 AM 15:00 STS-126 CREW ARRIVAL KSC 3:00 PM 4:00 PM 21:00 WEDNESDAY, NOVEMBER 12

! "#$ #%& Challenge the future. Delft University of Technology

Hazard Identification Questionnaire

Space Transportation Systems. System Concepts

July VA 219. ATV Georges Lemaître

Airport Compatibility Brochure 737 MAX. March 2014 PRELIMINARY

2.1 General Characteristics. 2.2 General Dimensions. 2.3 Ground Clearances. 2.4 Interior Arrangements. 2.5 Cabin Cross Sections

Worldwide Aircraft Services, Inc

RAAA Annual Convention This information is property of Embraer and cannot be used or reproduced without written permission.

The Regulatory Role of the

NASA Connection Free-Fall Rides

When most people build their avionics package,

KEY FEATURES IN SHORT

Space Based ADS-B. ICAO SAT meeting - June 2016 AIREON LLC PROPRIETARY INFORMATION

FOR REFERENCE ONLY NOT FOR FLIGHT

UH1H HP Modification and Upgrade Program

Ultra Long Range Jets

Airport Compatibility

EMBRAER PHENOM 100EV SN RANGE (NM) 1,178 PASSENGERS 6 MACH 0.70 CONTACT: GREG OSWALD I

Range Safety Concerns for Launching Winged Vehicles from Canaveral Spaceport

For the purposes of this guidance material the following definitions are used:

REPORT ACCIDENT. In-flight loss of control in a turbulent atmosphere, collision with vegetation, then the ground 1 - HISTORY OF FLIGHT

Spacecraft Avionics. Lecture #26 December 2, 2014 Avionics overview Shuttle systems Constellation systems MARYLAND U N I V E R S I T Y O F

Fuel Burn Reduction: How Airlines Can Shave Costs

SpaceCalc Shuttle Launch-and-Landing History

767 Airplane Characteristics for. Airport Planning. Boeing Commercial Airplanes. D SEPTEMBER 2005 i

S P E C I F I C AT I O N S

CUSTOM COMFORT AND ENHANCED PRODUCTIVITY A NEW CLASS OF AMENITIES

ATR FREIGHTER VERSIONS. AN EASY CONVERSION AVAILABLE SINCE 2002, TO EXTEND ATR s

Location: 2. It shows on at least two more places an example of the principle of dichotomy,

Aviation List. Admitted Liability: In aviation insurance, payments to an injured passenger made without the need of establishing liability.

Pilots, navigators, and engineers train at the USAF Test Pilot School preparing to write new chapters in aerospace history.

FAA Technical Documentation Requirements

Fuel 11. Upper Deck. Lower Deck

P310 VTOL UAV Operation Manual

ECLIPSE 500. Aircraft Overview. Do Not Use For Flight

THE LEADER IN PERFORMANCE AND EFFICIENCY

THE LEADER IN PERFORMANCE AND EFFICIENCY

TAKEOFF SAFETY ISSUE 2-11/2001. Flight Operations Support & Line Assistance

LAUNCH KIT. November 2017 VV11. MOHAMMED VI A satellite

Daher s TBM 930 makes its mark in the charter sector

Sub-Orbital Passenger Aircraft for Space Launch Operations

CIVIL AVIATION [(No. 18) STATE AIRCRAFT REGISTRATION AND MARKINGS] REGULATIONS, Arrangement of Regulations

NEXT GENERATION VERSATILITY

HARD. Preventing. Nosegear Touchdowns

FAA NextGENProgram & NEAR Laboratory. Massood Towhidnejad, PhD Director of NEAR lab

(a) This part prescribes rules governing the operation in the United States, of the following:

Gogo Connected Aircraft Services

CESSNA SKYMASTER 337

TAXIBOT. May Technical Partner

Low Cost Spacelift to LEO, GTO, and Beyond Using the OSP-2 Minotaur IV Space Launch Vehicle. Scott Schoneman, Lou Amorosi, Ron Willey, and Dan Cheke

WEDNESDAY, MAY 28 COUNTDOWN STATUS BRIEFING KSC 9:00 AM 10:00 AM 15:00 ISS EXPEDITION 17 COMMENTARY JSC 9:30 AM 10:30 AM 15:30

ONE-ENGINE INOPERATIVE FLIGHT

A Human Factors Approach to Preventing Tail Strikes. Captain Vern Jeremica Senior Safety Pilot Boeing Commercial Airplanes May 2004

The Boeing Company forecasts a market for the Asia-Pacific region of about 8,960 new airplanes worth US$1,130 billion for the 2009 to 2028 period.

ROBERT L. HOOT GIBSON CONSULTANT

Arianespace 2013 Organization, History and Programs

/-400ER Freighters

Agenda Item 1.17 Wireless Avionics Intra-Communications (WAIC)

D8ULTRA-EFFICIENT COMMERCIAL AIRCRAFT

K I N G A I R C 9 0 G T x

Dornier OE-LIR MSN 3115

2013 Taiwan Innovative Unmanned Aircraft Design Competition

ASTM International Committee F38 Unmanned Aircraft Systems. Michael J. Goy Defense Standardization Program Office

FLIGHT AND OPERATING MANUAL SUPPLEMENT FMS305902, REVISION 1 SEAPLANES WEST INC.

Airport Compatibility Brochure 737 MAX

East Coast Aero Club Renter Quiz

LIMA-PERU AUGUST 2011 Speaker: Jorge Rodríguez Coordinator SAR/RCC/SPOC /CENAMER CONTROL/COCESNA

Transcription:

Review of the Space Shuttle Program Karol Bo Bobko SEMWO 11 November 17, 2011

Shuttle Planning Planning for the Space Shuttle began before the Apollo Program was completed. The consensus was to develop an infrastructure in low earth orbit (LEO) consisting of a space station and an inexpensive, easy and efficient way to get to and from LEO. NASA didn t believe that they had the resources to build both the Shuttle and the Space Station at the same time so the Shuttle was chosen as the first project: The Space Station probably required a shuttle for construction The Space Shuttle could do other things such as launch satellites

Early Space Shuttle Designs Early designs were for a completely reusable shuttle. The first stage generally was a booster that flew back to the launch site. That proved to be complex and expensive. The option chosen had the two ocean recoverable solids as the first stage and the throw-away tank.

President Nixon Announces the Space Shuttle Program on January 5, 1972 Contract for construction of the shuttle Orbiter was awarded August 9, 1972. First main engine test October 17, 1975. Rollout of the orbiter Enterprise September 17, 1975. Two minute firing of the Solid Rocket Booster July 18, 1976. Approach and Landing Test first free flight August 12, 1976. Columbia launch April 12, 1981.

Approach and Landing Tests The Approach and Landing Tests were conducted between February and October 1977 at Edwards AFB in California The Shuttle was built at Palmdale and transported overland to Edwards The Shuttle was missing some systems that would be required to support a crew on a space flight There were three phases to the tests: Taxi tests Captive tests where the Shuttle stayed on the Shuttle Carrier Aircraft Captive inert tests where the Shuttle was unpowered Captive active tests where the Shuttle was powered up Captive active tests were practice flights for the free flights Free Flights where the Shuttle flew off the back of the SCA Tailcone on flights - Shuttle had a better glide ratio and less turbulence Tailcone off flights - approximated the landing trajectory of an operational orbiter

ALT Free Flight

ALT Landing

New Technologies There were a number of new technologies that were developed to allow the Space Shuttle to accomplish its mission Reusable, high performance main engines Reusable thermal protection system Fully integrated avionics and flight control system

Space Shuttle Main Engines (SSME) First flight April 12, 1981 Manufacturer Pratt & Whitney Rocketdyne Liquid-fueled engine Propellant LOX /Liquid Hydrogen Cycle Staged combustion Nozzle area ratio 77 Performance Thrust (Vac.) 2.1834 MN at 104.5% of design thrust Thrust (SL) 1.8 MN Chamber pressure 18.94 MPa at 100% power I sp (Vac.) 452.5 seconds I sp (SL) 363 seconds

Shuttle Engine Start

Shuttle Thermal Protection System Tile types High-temperature reusable surface insulation (HRSI) Fibrous Refractory Composite Insulation Tiles (FRCI) Toughened unipiece fibrous insulation (TUFI) Low-temperature reusable surface insulation (LRSI) Non-tile TPS Flexible Insulation Blankets (FIB) Reinforced Carbon-Carbon (RCC) Nomex Felt Reusable Surface Insulation (FRSI) Gap fillers

HRSI Space Shuttle Tiles Composed of high purity silica fibers 20,548 of these tiles mainly on the underside of the Orbiter Normally 15 X 15 cm Thickness 2.5 to 13 cm depending on heat ~ 140kg/m3 Black coating is Reaction Cured Glass Protects to 1260 C

Shuttle Avionics One of the leading edge technologies for its day. The Space Shuttle was completely digital fly-by-wire for all of the flight phases. Most of the avionics were typically redundant to allow fail-ops / fail safe operation. That meant that with one failure the system was still operational and with two failures it was safe. Fail-ops / fail safe required a sophisticated failure detection and reconfiguration system. The next slide will show a view of the cockpit. Remember this is a rocket, a space craft and an aircraft. To verify the operation of the avionics a Shuttle Avionics Integration Laboratory (SAIL) was constructed.

Shuttle Cockpit

Shuttle Avionics Integration Laboratory (SAIL) SAIL enables Orbiter hardware and flight software to be integrated and tested in a simulated flight environment. The testing process is extensive and rigorous; the software on the Shuttle is often considered to be among the most bug-free of operational systems. The laboratory contains a complete avionics mock-up of a Shuttle. The electronics are identical in position and type to those used on the Shuttle.

Space Shuttle Features Largely reusable Large cargo capacity (both volume and weight) Airlock Crew of seven (eight before the bail-out modifications) Robotic arm Approximately two weeks on orbit stay Ability to support payloads (electrical power, data, cooling) Return significant weight back to earth Large cross range

Space Shuttle Training NASA used a range of training techniques and training devices from books and lectures to sophisticated simulators. A new astronaut is called an Astronaut Candidate or Ascan. They go through a broad training course for about a year. After that they are assigned technical duties. During the Shuttle Program the astronauts were assigned to a crew about a year before launch. During that time they work to develop the skills that will be needed for their flight. About six months before flight they are relieved of other duties and focus on their flight. The Shuttle is a very complicated device that takes a lot of study and training.

Shuttle Training Aircraft Modified Gulfstream Shown here during a practice shuttle approach Note the main gear down to produce drag The nose gear is not stressed to be down at this speed Accurate simulation down to the pilot s eye height during landing Doesn t actually land during a simulated shuttle landing

Shuttle Mission Simulator Actually two simulators Motion base has only the front cockpit Fixed base has the entire crew compartment Primary simulator for integrated crew training Telemetry is sent to Mission Control Center (MCC) for integrated training with the MCC Crews spent hundreds of hours in this simulator

Neutral Buoyancy Laboratory It is 202 ft in length, 102 ft in width, and 40 ft in depth (20 ft above ground level and 20 ft below) and holds 6.2 million gallons of water.

Neutral Buoyancy Laboratory Crews practice underwater to try and simulate zero gravity. Used to develop procedures and allow astronauts to become familiar with the environment.

Provide the capability to develop procedures and train outside of the simulation facilities. Visible are the : Full Fuselage Trainer Crew Compartment Trainer Crew Compartment Trainer II. This mockup can be positioned in 7 orientations: Launch (nose up) Runway Nose down Side hatch up Side hatch down Horizontal Landing Space Vehicle Mockup Facility

Vertical Motion Simulator The VMS supplements the Shuttle Training Aircraft and the Shuttle Mission Simulator. The Shuttle Training Aircraft does not actually land and the Shuttle Mission simulator has very limited motion. The VMS provides shuttle approach and landing training, with good motion, all the way through roll-out to a stop.

Assembling the Shuttle for Launch The major parts of the Space Shuttle are brought to the Kennedy Space Center and assembled on the Mobile Launch Platform (MLP)in the Vehicle Assembly Building (VAB).

Mobile Launch Platform and Crawler The shuttle stack is assembled on the Mobile Launch Platform and transported to the launch pad on the Crawler/ Transporter.

Vehicle Assembly Building Assembly of the stack is accomplished in the Vehicle Assembly Building (VAB).

SRB Recovery Ship Freedom Star

Solid Rocket Boosters (SRB) The first element of the Shuttle stack is the SRB. These are brought by rail from Utah where they have been refurbished.

Segments of the SRB being joined together. When assembled each SRB weighs 1,300,000 pounds. Thrust at liftoff is 2,650,000 pounds. Solid Rocket Booster

External Tank The External Tank is transported from Mississippi to the launch site on a barge which travels on the Intercoastal Waterway. The External Tank holds 500,000 gallons of fuel and oxydizer.

Orbiter The Orbiter is maintained and readied for the flight in the Orbiter Processing Facility (OPF).

Orbiter in the VAB In the VAB a sling is attached to the Orbiter so it can be lifted, rotated and attached to the External Tank on the MLP.

Orbiter Lifted onto the External Tank The Orbiter is carefully lifted and joined to the external Tank. The orbiter will weigh about 250,000 pounds.

Shuttle in the VAB on the MLP

Shuttle Being Transported to the Launch Pad Crawler transporter has a max speed of 1.6 km/hr. Takes about 5 hours to get to the pad. Crawler transporter weighs 2.721 million kg. The Shuttle and MLP weigh 6.22 million kg. Fuel consumption is about 350 liters per kilometer.

Space Shuttle on the Launch Pad The left part of the structure contains the Payload Change-out Room (PCR) which can be rotated to fit next to the Shuttle and allow access to the Shuttle payload bay.

Payload Change-out Room (PCR) There is access to the payload bay when the Shuttle is on the launch pad. A room fits against the Shuttle to allow the Shuttle payload bay doors to be opened and have sheltered access to the payload bay. This picture is from inside the PCR and shows the Shuttle payload bay with the starboard payload bay door open.

Space Shuttle Ready for Launch

Mission Control Center (MCC)

The Shuttle Carried Many Payloads The Space Shuttle carried many payloads into orbit including: Earth satellites (Hubble, Gamma Ray, Chandra X-Ray) Deep space probes (Magellan/Venus, Galileo/Jupiter, Ulysses/Sun Polar) Experiment laboratories (Spacelab and Spacehab) Space Station elements (27 flights) Space Station logistics (9 Spacehab and 11 MPLM missions) Experiments Rendezvous (10 ) and docking (9) missions with Russian Space Station Mir Repair missions (5 Hubble repair missions plus two others) Communication satellites (6 TDRS among many others) In addition to the primary payloads there were also numerous smaller secondary payloads

Satellites Launch from Shuttle Before the Challenger accident the Shuttle launched numerous satellites. This picture is of the first Tracking Data Relay Satellite (TDRS) launched from STS 6. After the accident satellites were put on unmanned vehicles.

Spacelab in the Cargo Bay The first Spacelab was built by the European Space Agency in exchange for flight opportunities. This picture was taken on the first Spacelab flight STS 9. The Spacelab is in the Shuttle payload bay with the doors open. The connecting tunnel from the Shuttle cockpit to the Spacelab can be seen at the bottom of the picture.

Major Spacelab components were flown on 25 Shuttle flights. Interior of the Spacelab Module

Space Shuttle Approaching the ISS with a Multi Purpose Logistics Module (MPLM). 37 Shuttle flights have docked with the ISS

Hubble Space Telescope Repair There have been five servicing missions to the Hubble Space Telescope. These missions have replaced and repaired components of the telescope.

Shuttle Landing

Space Shuttle Statistics 5 space worthy orbiters: Columbia, Challenger, Discovery, Atlantis, Endeavour 135 flights into space More than 500,000,000 miles in space (more than 21,000 orbits) 852 total crew (355 individual fliers) 3,513,638 pounds of cargo launched into orbit Heaviest spacecraft deployed - 25 Tons (Chandra X-Ray Observatory) Longest Mission - 17 days, 15 hours, 13 minutes, 18 seconds