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Recent Development in Space Cheng-I Chen Presentation at GWS August 4, 2012.

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Presentation on theme: "Recent Development in Space Cheng-I Chen Presentation at GWS August 4, 2012."— Presentation transcript:

1 Recent Development in Space Cheng-I Chen Presentation at GWS August 4, 2012

2 Outline Introduction US Space Program Space Stations and ISS Space Transportation after Space Shuttle Mars and Moon Exploration Chinese Development Rocket and Satellite Program of North Korean Recent Development of NSPO ( credit NSPO )

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4 Education Development in 50 years

5 Key US Space Agencies It is more than NASA NASA Department of Defense USAF Space Command Other Military Services (Navy and Army) National Security Agency (SIGNAT signal intelligence) NGA (National Geospatial-Intelligence Agency) Department of Commerce NOAA National Weather Service National Envir Satellite, Data, and Information Service NRO National Reconnaissance Office ( DoD and CIA) Others –NSF, FAA, etc …

6 NASA’s Main Missions Aeronautics Research – Air Transportation – Air Traffic Control – Aeronautics Test Science – Earth – Heliophysics – Planets – Astropysics Human Exploration and Operations – ISS – Space Communication and Navigation – Launch Service – Commercial Space Transportation – Exploration System Development – Advanced Exploration Systems – Space Life Science Research and Application

7 Space Stations and ISS

8 Salyut 7 Space Station

9 Skylab Space Station

10 MIR Space Station

11 International Space Station (1) Cooperative Program among USA, Russia, ESA, Japan, and Canada First Russian Module ‘Zarya’ launched in November, 1998 Total of 15 pressured modules (US-7,Russia-5, Japan-2, ESA-1) in ISS now One more Russian module (MLM) is planned for 2013 Partners agreed to extend the life from 2015 to 2020

12 International Space Station (after STS-134 mission; Credit: NASA)

13 International Space Station (2) Life in ISS – Accommodate 6 astronauts normally – Expedition 32 crew are in residence now – Typical duty is 6 months in space AMS-2 was added by Space Shuttle flight STS- 134 in May 2011 Russia plans to use some of its ISS modules for the next generation space station OPSEK. Other modules are not planned to be reused.

14 Space Transportation Serve the need of reaching space Provide means of transportation between the earth and space stations Requirements and Design are Different for Crew and Cargo Transportation

15 Space Shuttle The first reusable spacecraft launched April 12, 1981 with Columbia. NASA has lost Columbia and Challenger in fatal disasters. Three others (Discovery, Atlantis and Endeavour) retired in 2011. The Soviets developed their own reusable craft, Buran Buran flew only once, on November 15, 1988, when it spent 3.5 hours in space, orbited the earth twice, and landed, all under remote control

16 Space Shuttle US Space Shuttle (year 1981-2011) Six shuttles were built (1 test 5 operations) Total of Missions : 135 mission (plus 6 test flights of Enterprise) Oribital Weight : 78 tons Crew Capacity - 7 Cargo Capacity - 24.4 tons Russia(Burun), ESA, and Japan all terminated their shuttle programs before completion

17 Space Development in the past 50 years

18 US Commercial Space Transportation US Gov’t turns to commercial space transportation after Shuttle Major programs: – Space XFalcon 9 and Space Dragon – OSC/Thales Alenia SpaceAntares and Cygnus – Lockheed Martin-led TeamDelta IV and Orion Other Programs – Virgin Galactic SpaceShip Two (suborbital flight for tourists) – BigelowOrion Lite – Sierra Nevada Dream Chaser – Blue OriginNew Sheppard – BoeingCST-100

19 View from the International Space Station of the SpaceX Dragon spacecraft as the station's robotic arm moves Dragon into place for attachment to the station. May 25, 2012. Photo: NASA

20 SpaceX’s Space Dragon Successful demonstration flight in May 2012 Fully autonomous rendezvous and docking (with manual override capability in crewed configuration ) 6,000 kg (13,228 lbs) payload up-mass to LEO; 3,000 kg (6,614 lbs) payload down-mass Payload Volume: 10 m3 (350 ft3) pressurized, 14 m3 (490 ft3) unpressurized Dragon is 4.4 meters (14.4 feet) tall and 3.66 meters (12 feet) in diameter. The trunk is 2.8 meters (9.2 feet) tall and 3.66 meters (12 feet) wide. Supports up to 7 passengers in Crew configuration

21 Major Components of Space Dragon (credit SpaceX)

22 Non-US Space Vehicles Russian Spacecraft Soyuz Progress PPTS and Advanced Crew Vehicles (in development) ESA ATV CSTS and ACTS (in development) Japan HTV China Shunzhou India ISRO Orbital Vehicle (in development)

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25 Recent Mars Exploration US – MERS-A Sprit Dover(2003-2011) – MERS-B Opportunity Dover(2003-now) – Mars Reconnaissance Orbiter (2005-now) – Phoenix (Lander)(2007-2008) – Dawn (Gravity assist to Vesta)(2007-now)Vesta ESA – Rosetta (Gravity assist enroute to comet 67P/Churyumov-Gerasimenko)(2004-now) 67P/Churyumov-Gerasimenko

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27 Recent Mars Exploration NASA Phoenix The Phoenix lander descended on Mars on May 25, 2008. Mission scientists used instruments aboard the lander to search for environments suitable for microbial life on Mars, and to research the history of water there.landermicrobiallife on Mars The program was a partnership of many US and European Universities and a number of space agencies and aerospace companies

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29 Recent Mars and Asteroid Exploration NASA’s Dawn It was launched in 2007 toward Mars to get gravity assisted flyby and to orbit around dwarf planet Vesta from July 16, 2011 to August 26, 2012. The spacecraft will then head to Ceres, which it is scheduled to reach in February 2015. It is propelled by three xenon ion thrusters and can produce velocity change of 10km/secxenonion thruster

30 Vesta, Ceres and Earth's MoonCeresMoon with sizes shown to scale

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33 New Mars Exploration NASA’s Mars Science Laboratory NASA's MSL, with its Martian rover named "Curiosity", was launched on November 26, 2011 and contains instruments designed to look for past or present conditions relevant to habitability. The Curiosity is scheduled to land on Mars in August 5, 2012 at 10:31 pm PDT NASAMSLCuriosity Cost of Mission: $2.5B

34 Mars Science Laboratory Landing of Curiosity Cruise Distance: 354 million miles Distance to Earth: 154 million miles Communication Delay: 14 minutes Touch Down Operation: 7 minutes Touch Down Phase: – S-Curve Maneuver (13000 mph->900mph) – Parachute (to about 1 mile altitude) – Rocket Burn (slow down to 2 mph) – Hovering,Spool Cable to lower the Curiosity – Cut Cables

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38 Curiosity's Landing on Mars

39 Viedo of Curiosity’s Final Arrival SHOW VIEDO

40 Recent Mars Exploration Russia’s Fobos-Grunt Lander In September 2011, Roscosmos' Fobos-Grunt lander with sample return was launched.Fobos-Grunt It is intended to obtain surface samples from the Martian moon PhobosPhobos The Fobos-Grunt mission suffered a complete control and communications failure during launch and was left stranded in low Earth orbit and later falling back to Earth.

41 Recent Mars Exploration CNSA’s Yinghhou 螢火 1 Launched on November 8, 2011, Yinghou-1 was Chinese first Mars-exploration space probe It was launched along with the Russian Fobos- Grunt sample return spacecraft and intended to orbit Mars for around two years, studying the planet's surface, atmosphere, ionosphere and magnetic field.RussianFobos- Gruntsample returnionospheremagnetic field Burns to depart Earth orbit fialed

42 Future Mar Exploration NASA’s MAVEN Mars Atmosphere and Volatile EvolutioN (MAVEN) is the only currently planned NASA’s future Mars exploration mission The planned mission will send a space probe to orbit Mars and study its atmospherespace probe Mars It will help determine what caused the atmosphere —and water— to be lost to space atmospherewater To be launched in late 2013 and reaches Mars in Fall of 2014

43 Future Mar Exploration ESAExoMars 2016-2018 The EAS-led program is originally joined by NASA and Russia NASA backed out due to funding problem Mission 2016 - The Gas Orbiter and EDM Lander Mission 2018 – Lander and Rover

44 ESA ExoMars 2016 Artist's concept of the ExoMars 2016 spacecraft, which consists of the Trace Gas Orbiter and the Entry, descent and landing Demonstrator Module (EDM). CREDIT: ESA-AOES Medialab

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46 Chinese Space Development Overview Launch Vehicles Manned Space Program Chinese Space Station Moon Exploration Navigation Satellites

47 Chinese Space Development Overview

48 Chinese Space Development Recent Major Milestone October 15, 2003 China‘s 1 st Manned Mission Shenzhou-5 October 12, 2005 Launched 2 nd Manned Mission September 2008 First Space Walk on 3 rd Manned Mission September 2011 Launched Tiangong-1,an Unmanned Rendezvous Module November 2011 Completed a docking of the Shenzhou-8 with the Tiangong 1 by remote control 2012 June 16 launched Shenzhou-9 with 3 Astronauts to Dock with Tiangong 1 automatically and manually

49 Chinese Launch Vehicles Long March Families Name Status Stages LEO (kg) GTO(kg) Long March 1Retired3 300- Long March 1 Long March 1DRetired3 930- Long March 1D Long March 2ARetired2 1,800- Long March 2A Long March 2CActive2 2,400- Long March 2C Long March 2DActive2 3,100- Long March 2D Long March 2ERetired2 (plus 4 Strap-on boosters)9,5003,500 Long March 2E Long March 2E(A)In development2 (plus 4Strap-on boosters)14,100- Long March 2E(A) Long March 2FActive 2 (plus 4Strap-on boosters)8,4003,370 Long March 2F Long March 2F/GActive 2 (plus 4 Strap-on boosters)11,200N/A Long March 2F/G Long March 3Retired3 5,0001,500 Long March 3 Long March 3AActive 3 8,5002,600 Long March 3A Long March 3BRetired? 3 (plus 4 Strap-on boosters)12,0005,100 Long March 3B Long March 3B(A)In development 3 (plus 4Strap-on boosters)3,0006,000 Long March 3B(A) Long March 3B/EActive 3 (plus 4 Strap-on boosters)?5,500 Long March 3B/E Long March 3CActive 3 (plus 2 Strap-on boosters)?3,800 Long March 3C Long March 4ARetired 3 4,000(SSO) 1,500 Long March 4ASSO Long March 4BActive 3 4,200(SSO) 2,200 Long March 4B Long March 4CActive 3 4,200(SSO) 2,800 Long March 4C Long March 5In development 3 25,00014,000 Long March 5 Long March 6In development 3 (SSO) 500 Long March 6

50 Long March II-F rocket transported to the launch pad. Image released June 11, 2012. CREDIT: China Manned Space Engineering

51 Launch History of CZ-2F Date & Time (GMT)PayloadOutcomeRemarksGMT 19 November 1999, 22:30Shenzhou 1SuccessFirst unmanned test of the Shenzhou capsuleShenzhou 1Shenzhou 9 January 2001, 01:00Shenzhou 2SuccessSecond unmanned test of the Shenzhou capsule, carried live animalsShenzhou 2 25 March 2002, 14:00Shenzhou 3SuccessThird unmanned test of the Shenzhou capsule.Shenzhou 3 29 December 2002, 16:40Shenzhou 4SuccessFinal unmanned test of the Shenzhou capsule.Shenzhou 4 15 October 2003, 01:00Shenzhou 5SuccessChina's first manned spaceflightShenzhou 5 12 October 2005, 01:00Shenzhou 6SuccessSecond manned spaceflight, first with two crew membersShenzhou 6 25 September 2008, 13:10Shenzhou 7SuccessThird manned spaceflight, first with three crew members, first to feature Extra-vehicular activityShenzhou 7Extra-vehicular activity 29 September 2011, 13:16Tiangong 1SuccessThe first Chinese space station, with a modified version of Long March 2FTiangong 1Chinese space station 31 October 2011, 21:58Shenzhou 8SuccessUnmanned spaceflight to test automatic rendezvous and docking, with a modified version of Long March 2FShenzhou 8 rendezvousdocking 16 June 2012 18:37 Shenzhou 9Success Manned spaceflight to test automatic and Manual rendezvous and docking, with a modified version of Long March 2F rendezvousdocking

52 CZ-2F (LM-2F) Function: Man-rated orbital launch vehicleMan-ratedorbitallaunch vehicle Manufacturer Country of Origin: ChinaChina SizeHeight: 62 meters (203 ft) Diameter: 3.35 meters (11.0 ft) Mass: 464,000 kilograms (1,020,000 lb) Stages: 2 Capacity Payload to LEO: 8,400 kilograms (19,000 lb)LEO Associated Rockets Family: Long MarchLong March Launch History Status: Active Launch Sites :, JSLCJSLC Total launches:10 Successes: 10 Maiden flight: 19 November 1999

53 Shenzhou spacecraft China’s Shenzhou spacecraft are derived from the three-module Soyuz spacecraft built by Russia. They consist of an orbital module, a crew capsule and a propulsion module. But unlike Russia’s Soyuz, the Shenzhou’s orbital module has its own solar arrays, allowing it to linger in orbit for months after its crew has returned to Earth.

54 3 Modules of Shenzhou Spacraft

55 Shenzhou Series Shenzhou 1 – November 19, 1999 – unmanned test flight Shenzhou 1 Shenzhou 2 – January 9, 2001 – carried animals Shenzhou 2 Shenzhou 3 – March 25, 2002 – carried a test dummy Shenzhou 3 Shenzhou 4 – December 29, 2002 – carried a test dummy and several science experiments Shenzhou 4 Shenzhou 5 – October 15, 2003 – 14 Earth orbits carrying Yang Liwei Shenzhou 5Yang Liwei Shenzhou 6 – October 12, 2005 – five day mission with Fei Junlong and Nie Haisheng Shenzhou 6Fei JunlongNie Haisheng Shenzhou 7 – September 25, 2008 – three man crew with Zhai Zhigang, Liu Boming, and Jing Haipeng; spacewalk performed by two crew members Shenzhou 7Zhai ZhigangLiu BomingJing Haipengspacewalk Shenzhou 8 – October 31, 2011 – unmanned mission carrying 2 test dummies, which rendezvoused and docked with Tiangong-1. Shenzhou 8Tiangong-1 Shenzhou 9 – June 16, 2012 – three-person crew (one female), docked with Tiangong-1. The spacecraft returned to earth on 29 June 2012 with three crew members appearing in good health. Shenzhou 9

56 Photo of the Shenzhou 8 spacecraft undergoing testing earlier in 2011. CREDIT: China Manned Space Engineering Office View full size image

57 Chinese Space Station September 29, 2011, China launched Tianggong 1, later docked with Shenzhou 8 and Shenzhou 9 Tiangong-2 is scheduled to be launched around 2013. It weights about 20 tons Tiangong-3 will be launched around. It weights about 22 tons Chinese Space Station will consist of one Core Cabin Module and two Laboratory Cabin Module and weight about 65 tons. It will launch in the 2020-2022 timeframe and and will support three astronauts for long-term habitation. Resupply craft and manned Shenzhou craft will be able to provide needed space transportation

58 Tiangong 1 and Shenzhou 9

59 Docking and Berthing Technical Issues Related to Berthing & Docking – Orbital Adjustment – Attitude Alignment – Ranging – Approach and Capture – Date Interface

60 Docking Interface Two basic types of docking system – Non-androgynous Docking System (Used by most earlier Russian System for automatic docking) Role can not be switched – Aandrogynous Docking System (Used in more recent system, including international programs) Active and Passive role can be switched Allow cascade docking – Docking Adaptor can be used

61 Docking Interface There are many standard docking interfaces: – Docking Adaptor can be used – There are a lot of plugs for gas and electrical circuits that must be perfectly aligned," s must also be precisely positioned to be connected

62 Docking Accident of MIR with Progress in 1997 Progress smashed into Solar Panel and wall of Spektr Module during manual docking, causing it to depressured. MIR lost half of its power due to solar panel damage and the pressured module Spetkr containing half of US experiments was also abandoned

63 Docking of Shenzhou with Tiangong Similar to the Russian-designed APAS system, used in Apollo-Soyuz Test Project, the Russian Mir Space Station, and by Space Shuttles visiting ISS Shenzhou is the Active Vehicle for docking Automatic docking is demonstrated in Shenzhou 8 mission and manual docking is performed in Shebzhou 9 with crew on-board There are a lot of plugs for gas and electrical circuits that must be perfectly aligned," s must also be precisely positioned to be connected

64 Viedo of docking

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67 Chinese Lunar Exploration Plan First phase lunar program ( 嫦娥 -1) — launched in 2007 with CZ-3A: two lunar orbital probesCZ-3A Second phase lunar program ( 嫦娥 -2)— to be launched in 2012 with CZ-5/E:first Moon landing of a couple of roversCZ-5/E Third phase lunar program ( 嫦娥 -3) — to be launched in 2017 with CZ-5/E: automated Moon landing and return sampleCZ-5/E Fourth phase lunar program ( 嫦娥 -4) — to be launched in 2024 with CZ-7: crewed missionCZ-7

68 Chinese Navigation Satellite Beidou System Total Satellites: 35 (expected in 2020) Coverage: Asia now and global in 2020 Orbital: High and Medium Possition Accuracy (civil): 10m Velocity Accuracy: 0.2m/sec Timing accuracy: 0.02 msec

69 North Korean Satellite Launch Designation DateLaunch Site PayloadRemark Taepodong-2 4 July 2006 [1 TonghaeUnknown Failed early in flight, possibly intended to be suborbital [1 Tonghaesuborbital Unha-25 April 2009TonghaeKwangmyŏngsŏng-2 Failed to reach orbitTonghaeKwangmyŏngsŏng-2 Unha-313 April 2012SohaeKwangmyŏngsŏng-3Failed to reach orbitSohaeKwangmyŏngsŏng-3

70 Due to the secrecy of North Korea's ballistic missile program, technical details are scarce. According to several analysts the Unha's first stage consists of four clustered Nodong motors, which themselves are enlarged Scud motors. The second stage is supposed to be based on SS-N-6 technology North Korea is known to have acquired. The third and last stage might be identical to the Iranian Safir's second stage which is propelled by two small gimbaled motors. Also North Korea has probably not yet developed a nuclear warhead small enough to be fit on their ballistic missiles.NodongScudSS-N-6Safir's

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72 History of NASA's annual budget (millions of US dollars)NASA Year NASA budget (Nominal)(in $Millions) % of Fed Budget [4][5] 2007 Constant Million Dollars 1958 89 0.1% 488 1959 145 0.2% 1,841 1960 401 0.5% 3,205 1961 744 0.9% 6,360 1962 1,257 1.18% 12,221 1963 2,552 2.29% 24,342 1964 4,171 3.52% 33,241 1965 5,092 4.31% 33,514 1966 5,933 4.41% 32,106 1967 5,425 3.45% 29,696 1968 4,722 2.65% 26,139 1969 4,251 2.31% 21,376 1970 3,752 1.92% 18,768 1971 3,382 1.61% 15,717 1972 3,423 1.48% 15,082 1973 3,312 1.35% 14,303 1974 3,255 1.21% 11,494 1975 3,269 0.98% 11,131 1976 3,671 0.99% 11,640 1977 4,002 0.98% 11,658 1978 4,164 0.91% 11,411 1979 4,380 0.87% 11,404 1980 4,959 0.84% 11,668 1981 5,537 0.82% 11,248 1982 6,155 0.83% 11,766 1983 6,853 0.85% 13,051 1984 7,055 0.83% 13,561 1985 7,251 0.77% 13,218 1986 7,403 0.75% 13,421 Year NASA budget (Nominal) % of Fed Budget [4][5] 2007 Constant Million Dollars 1987 7,591 0.76% 17,735 1988 9,092 0.85% 14,454 1989 11,036 0.96% 16,734 1990 12,429 0.99% 18,019 1991 13,878 1.05% 19,686 1992 13,961 1.01% 15,310 1993 14,305 1.01% 18,582 1994 13,695 0.94% 18,053 1995 13,378 0.88% 16,915 1996 13,881 0.89% 16,457 1997 14,360 0.90% 15,943 1998 14,194 0.86% 15,521 1999 13,636 0.80% 15,357 2000 13,428 0.75% 14,926 2001 14,095 0.76% 15,427 2002 14,405 0.72% 15,831 2003 14,610 0.68% 16,021 2004 15,152 0.66% 15,559 2005 15,602 0.63% 16,016 2006 15,125 0.57% 16,085 2007 15,861 0.58% 15,861 2008 17,318 0.60% 17,138 2009 [6] 17,782 0.57% 17,186 2010 [7] 18,724 0.52% 17,804 2011 [8] 18,448 0.53% 17,005 2012 (est.) [8] 17,770 0.48% 16,014 2013 (proj.) [8] 17,711 2014 (proj.) [8] 17,711 2015 (proj.) [8] 17,711 Notes: Sources: U.S. Office of Management and Budget (OMB) (needs proper citation-link, numbers here differ from NASA Pocket Statistics),NASA [4][5]NASA [4][5] [6] [7] [8] U.S. Office of Management and Budget

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74 National GDP in 2004 Percent spent on space USA 11.8 trillion 0.14% (NASA) Europe 11.7 trillion 0.03% (not inc. individual agencies) Japan 3.7 trillion 0.05% China 7.3 trillion 0.02% Russia 1.4 trillion 0.06% India 3.3 trillion 0.03% Taiwan (2011) 0.4 Trillion 0.01%

75 Thank You For Your Attention SPACE is The Frontier of Today and Tomorrow


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