Tuesday, December 27, 2011

News & Events in Space Technology (December 27, 2011)



Launch of Russian Proton-M carrier rocket postponed
Moscow (RIA Novosti) Dec 27, 2011 - The launch of a Russian Proton-M carrier rocket with a Dutch telecommunications satellite SES-4 (NSS-14) onboard was called off on Monday due to "technical problems", a spokesman for the Khrunichev State Research and Production Center said. He said the new date for launch was being discussed. He did not elaborate on the cause of the delay. The launch would have been the 70th commerci ... more

Siberian man miraculously unharmed as satellite piece crashes through roof
Moscow (RIA Novosti) Dec 27, 2011 - A Siberian resident miraculously escaped serious injury or even death when a fragment of a Russian communication satellite crashed through the roof of his house. A Meridian satellite that was launched on Friday from the Plesetsk space center in northern Russia on board a Soyuz-2 carrier rocket crashed near the Siberian city of Tobolsk minutes after liftoff. Eight satellite fragments ... more

TECHNOLOGY TRENDS:

  • Either water or liquid nitrogen levels can be measured within 1-mm spatial resolution and 1°C up to a distance of 70 m from the optical interrogation unit. An innovative fiber-optic sensor has been developed for low-thrust-level settled mass gauging with measurement uncertainty <0.5 percent over cryogenic propellant tank fill levels from 2 to 98 percent. The proposed sensor uses a single optical fiber to measure liquid level and liquid distribution of cryogenic propellants. Every point of the sensing fiber is a “point sensor” that not only distinguishes liquid and vapor, but also measures temperature. This sensor is able to determine the physical location of each “point sensor” with 1-mm spatial resolution. Acting as a continuous array of numerous liquid/vapor point sensors, the truly distributed optical sensing fiber can be installed in a propellant tank in the same manner as silicon diode point sensor stripes using only a single feed-through to connect to an optical signal interrogation unit outside the tank. MORE

  • Purge Monitoring Technology for Gaseous Helium (GHe) Conservation
    John C. Stennis Space Center provides rocket engine propulsion testing for the NASA space programs. Since the development of the Space Shuttle, every Space Shuttle Main Engine (SSME) has gone through acceptance testing before going to Kennedy Space Center for integration into the Space Shuttle. The SSME is a large cryogenic rocket engine that uses Liquid Oxygen (LO2) and Liquid Hydrogen (LH2) as propellants. Due to the extremely cold cryogenic conditions of this environment, an inert gas, helium, is used as a purge for the engine and propellant lines since it can be used without freezing in the cryogenic environment. MORE

  • Storage, Distribution, and Conservation of Fluids (Cryogens, Liquids, Gases) Hydrogen is an inherently dangerous gas due to its combustibility and invisible flame. Area sensors only detect the presence, not the source of a hydrogen leak. This presents problems in high wind environments such as launch pads where a leak may not be detected at all. The Hydrogen Tape, developed in collaboration with the Florida Solar Energy Center, overcomes these limitations by providing users with an easily deployable visual indication system that can precisely pinpoint the leak. This tape can effectively identify leaks in pipe flanges and connections that area sensors and flame cameras may miss. Work is also underway at KSC to develop HyperTape, a tape that can visually detect the presence of hypergols, another dangerous but ubiquitous chemical. KSC researchers were able to achieve between 25-50 percent reductions in thermal heat transfer without greatly affecting the mechanical properties or processing conditions of Aerogel composite materials when compared to the base materials. This approach is important to reduce weight of lunar habitat systems, cryogenic storage tanks, and piping where weight and thermal conductivity are crucial to mission success. MORE

Sunday, December 25, 2011

ELECTRICAL, ELECTRONICS & COMMUNICATION ENGINEERING RESOURCES ON WEB

TECHNICAL REPORTS OF YOUR INTEREST

WEB RESOURCES FOR CHEMICAL ENGINEERS

Web sites & Portals on Structural and Civil Engineering

Friday, December 23, 2011

LITERATURE & WEBSITES & PORTALS OF YOUR INTEREST

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NASA Technical Standards :

The NASA Technical Standards Program (NTSP) is sponsored by the Office of the NASA Chief Engineer.The primary mission is the enhancement of NASA's engineering capabilities by providing technical standards required to meet the needs of the Agency. The NTSP provides NASA single point access to technical standards, tools, and best practices, national and international organizations.

Links:
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MIL  and DOD standards 'search & retireve' site:

This site provide the ability to locate Defense and Federal specifications and standards obtained from the official DoD repository, the ASSIST database. It searchable by standard number, by keyword or even by the status of publication.  You may execute a search by performing a few steps: Link

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Full-Text Technical Reports - A REFERRAL SITE
This site lists some of the web pages, where from you can get directed to a number of sources hosting fulltext reports. Pl try. -LINK

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WEB SITES & PORTALS OF YOUR INTEREST :
(this is not an exhaustive list)


       
Rocket Propulsion:

    NEWS & EVENTS IN SPACE TECHNOLOGY (Dec. 23, 2011)


    Soyuz rocket falls in Siberia after launch mishap
    Dec 23 -
    A Russian communications satellite failed to reach orbit Friday after the failure of the upper stage of its Soyuz rocket, the latest in a string of Russian launch failures. The Soyuz 2-1b rocket lifted off from the Plesetsk Cosmodrome in northern Russia at 7:08 am EST (1208 GMT, 4:08 pm Moscow time) carrying a Meridian communications satellite. While the launch initially appeared to go well, Russian officials later said the satellite failed to reach orbit and instead crashed in Siberia. Initial reports indicated a problem with the rocket's third stage. The launch failure is the fifth in just over a year for Russia, including the loss of a Progress cargo spacecraft on another Soyuz rocket in August. In addition, Russia's Phobos-Grunt Mars spacecraft was successfully launched in November, but was stranded in Earth orbit because of an unknown problem with the spacecraft. FULL STORY


    Final Chinese launch tally surpasses U.S. rocket fleet
    For the first time since the dawn of the space age, China's Long March rocket family eclipsed the annual flight rate of the U.S. fleet of space launchers Thursday with the successful deployment of a high-resolution mapping satellite. FULL STORY

    Cosmic Fail! Biggest Space Flops of 2011

    Rockets have been launching people, robots and satellites into space for more than 50 years. But major failures still occur, highlighting just how hard it is to escape the bonds of Earth on a rocketship bound for orbit. The year 2011 saw its share of launch and mission failures; thankfully, none of them involved astronauts. Here's a recap of the biggest space disappointments of the year: More...

    Kepler discovers first Earth-sized planets around Sun-like starsDec 21, 2011 : Astronomers announced Tuesday the discovery of the first planets similar in size to the Earth around a Sun-like star. The planets, designated Kepler-20e and Kepler-20f, orbit a Sun-like star 1,000 light-years away. Kepler-20e has a radius of 0.87 Earth radii, making it slightly smaller than Venus, while Kepler-20f is slightly larger, at 1.03 Earth radii. The two planets closely orbit their star, with orbital periods of 6.1 and 19.6 days, putting them well inside the star's habitable zone. Scientists hailed the discovery, though, as the first time a planet as small as the Earth has been found around a star similar to the Sun. The discovery was made using data collected by NASA's Kepler spacecraft as it observed transits of the planets across the star. Three other planets, larger than Earth but smaller than Neptune, have aslo been detected in Kepler observations of the star.Related Links: NASA press release    ;  SPACE.com article ;

    China launches communications satellite for Nigeria
    Dec 20, 2011 -  A Chinese rocket placed into orbit Tuesday a new communications satellite for Nigeria. The Long March 3B lifted off from the Xichang Satellite Launch Center at 11:41 am EST monday (1641 GMT Monday, 12:41 am Beijing time Tuesday) and placed the Nigcomsat-1R satelite into geosynchronous transfer orbit. The satellite, built by China Academy of Space Technology, will replace an existing Chinese-built communications satellite for Nigeria that failed in orbit in 2008. The 5,100-kilogram satellite will operate at 42.5 degrees east in GEO, providing communications services in several frequency bands for Nigeria.
    Related Link: Spaceflight Now article

    Still more than two months until next Ariane 5 launch
    Arianespace is readying the first Ariane 5 for launch in 2012 from French Guiana following delivery of this heavy-lift workhorse by its industrial prime contractor, Astrium.
    The Ariane 5 ES vehicle is now in the Spaceport's Final Assembly Building following its transfer from the Launcher Integration Building - where it underwent integration of its core cryogenic stage, solid propellant boosters, equipment bay and EPS upper stage.
    This version of Arianespace's workhorse heavy-lift launcher is now ready to receive its payload: the third Automated Transfer Vehicle (ATV) cargo resupply vessel developed by Europe for servicing of the International Space Station.
    The latest ATV is named after Italian physicist Edoardo Amaldi and will carry an estimated 6,960 kg of dry cargo, propellant, water and gas when it lifts off on 9 March 2011 from French Guiana.
    Arianespace is entrusted with the orbiting of ATVs under contract to the European Space Agency. The company lofted the first ATV (named after Jules Verne) in March 2008, which was followed by the launch of ATV Johannes Kepler in February 2011.
    The ATV launch will mark the end of an almost half-year long hiatus in Ariane 5 launches. The last Ariane 5 launch was that of Arabsat 5C and SES 2 on 21 September 2011. Moreover, details regarding the next commercial Ariane 5 launch have not been announced yet. It is not expected to occur before April 2012, though. According to earlier reports, Arianespace is facing growing problems finding matching satellite pairs to fit with their dual launch strategy. Source: Arianespace PR

    NASA, Industry discuss new booster development for Space Launch System
    On 15 December, more than 120 aerospace industry leaders from more than 70 companies attended the Space Launch System's Advanced Booster Industry Day held at Marshall Space Flight Center in Huntsville, Alabama. The event focused on a NASA Research Announcement for the Space Launch System's (SLS) advanced booster.
    Marshall is leading the design and development of the SLS on behalf of the agency. The new heavy-lift launch vehicle will expand human presence beyond low-Earth orbit and enable new missions of exploration across the solar system.
    For explorations beyond the first two test flights, the SLS vehicle will require an advanced booster with a significant increase in thrust over existing U.S. liquid or solid boosters.
    Through this research announcement, NASA is seeking proposals for engineering demonstrations and/or risk reduction strategies for advanced booster concepts. The aim is to reducing risks while enhancing affordability, improving reliability and meeting our performance goals during an initial 30-month phase prior to the full and open Design Development Test and Evaluation (DDTE) competition. The total award value for the research announcement is US$200 million with multiple awards anticipated.
    NASA anticipates initiating a full and open competition for the advanced booster system in FY2015 with award anticipated in FY2016 and hardware delivery in the FY2019 timeframe. The 130-metric-ton, evolved SLS is slated for completion following the 2021 test flight.
    Reference: NASA PR

    Sunday, December 18, 2011

    NEWS & DEVELOPMENTS IN SPACE TECHNOLOGY


    Soyuz launches six satellites from Kourou
    Soyuz launch of Pleiades 1A from Kourou (Arianespace)Sat, Dec 17 - A Soyuz rocket lifted off from Kourou Friday night, placing six French and Chilean satellites into orbit. The Soyuz STA rocket lifted off from Kourou, French Guiana, at 9:03 pm EST Friday (11:03 pm local time Friday, 0203 GMT Saturday) and placed its payload of six satellites into Sun-synchronous orbit over the next three and a half hours. The launch's primary payload was the Pléiades 1A imaging satellite, built by EADS Astrium with a camera provided by Thales Alenia Space. The one-ton satellite is operated by the French space agency CNES and will be used to provide high-resolution Earth images for civil and military applications. Also on the Soyuz were four Electronic Intelligence by Satellite (ELISA) signals intelligence satellites, each weighing 120 kilograms and built by Astrium and Thales, for the French military. The Soyuz also placed into orbit the 117-kilogram Sistema Satelital de Observación de la Tierra (SSOT) Earth imaging satellite built by Astrium for the Chilean government. The launch was the second time a Soyuz has flown from Kourou, after the inaugural Soyuz launch in October that carried two Galileo navigation satellites.
    Related Links:
     NASASpaceFlight.com, BBC article, Reuters article







    Phobos-Grunt expected to reenter next month
    Phobos-Grunt illustration (Roscosmos)Dec 18 - Russian officials now believe the Phobos-Grunt spacecraft, stranded in Earth orbit since its launch in early November, will reenter some time next month. Officials said late in the week that they expect the spacecraft to reenter between January 6 and 19 based on the current delay of its orbit, an estimate that agrees with outside analysis of the spacecraft's changing orbit. The Mars-bound spacecraft was launched in early November, but controllers lost contact with the spacecraft shortly after entering orbit, and the spacecraft's engines failed to fire to boost the spacecraft towards Mars. Efforts to restore communications with the spacecraft have failed, although an ESA ground station did detect signals from the spacecraft for a brief time in late November. Russian officials have given up hope of restoring control of the spacecraft before its reentry.
    Related Links: RIA Novosti article

    First navigation signals heard from Galileo satellite
    Engineers are analyzing the first signals from a Galileo navigation satellite after its payload began switching on last week for testing, according to the European Space Agency.    FULL STORY



    Soyuz rocket rolls out for next South American launch
    The second Soyuz rocket to fly from the commercial launch base in Kourou, French Guiana made a short but meaningful trip Monday when it was rolled from the assembly hangar to the pad and rotated to stand up vertically. PHOTO GALLERY 

    Wednesday, December 14, 2011

    News in Space Technology


    Taurus-2 rocket gets new name as Antares, as debut launch nears

    December 12, 2011- Orbital Sciences has rebranded its new commercial rocket that will ferry provisions and equipment to the International Space Station starting next year -- changing the booster's name from the Taurus 2 to Antares. The first launch is planned for February from the pad under construction at Wallops Island, Virginia. That will be a qualification test-flight of the rocket in advance of launching a NASA-sponsored demonstration later in the spring to propel the Cygnus cargo ship to a linkup with the space station.
    The company has been working on the new rocket for four years, bringing the design to fruition for entrance into the medium-size payload market of the launch industry. Orbital's other rocket lines -- Pegasus, Taurus XL and Minotaur -- are suited for smaller satellites and cargo weights.
    The Taurus XL, which shared virtually no commonality with the Taurus 2, suffered back-to-back launch failures when its nose cone didn't separate during a pair of NASA environmental satellite-deployment missions from Vandenberg Air Force Base in the past two years.
    Giving the Taurus 2 a new name certainly won't hurt breaking any links in public perceptions with the Taurus XL.
    In announcing the new name, Orbital said it made the move "to clear up any marketplace confusion and provide clear differentiation between this new launch vehicle and our Taurus XL rocket."
    "Antares is significantly different - it serves the medium-class space launch market and its liquid fuel first stage technology is major departure from previous Orbital space launch vehicles. In addition, a project of this scale and significance deserves its own name like Orbital's Pegasus, Taurus and Minotaur rocket programs that have come before it," the company said. The name Antares comes from the "supergiant" star located in the constellation Scorpius and has a red hue when observed by the naked eye. It was picked, Orbital says, because it "is one of the brightest stars in the skies and we expect the Antares rocket to be one of the brightest stars in the space launch vehicle market. Orbital selected the name in keeping with the company's tradition of using Greek-derived celestial names for launch vehicles."
    Antares is a two-stage rocket combined of liquid- and solid-propellant motors. The kerosene and liquid oxygen-fed first stage is equipped with two AJ26-62 powerplants from Soviet stockpiles that U.S. engine-maker Aerojet has prepped for use. Tanks and assembly of the stage structures are provided by firms in the Ukraine that also make the successful Zenit launcher. Antares' second stage is a solid-fuel Castor 30B motor produced by ATK. Following the two test flights in the first half of 2012, Antares will begin a series of operational Cygnus resupply missions to the International Space Station later in the year. NASA has awarded Orbital a deal covering 8 flights valued at $1.9 billion to deliver cargo to the orbiting outpost through 2015 in a commercial arrangement that replaces the retired space shuttles for hauling supplies.
    Under the Commercial Orbital Transportation Services project, or COTS, NASA invested seed money with Orbital and SpaceX to develop the means of trucking cargo to the station.
    Orbital's COTS deal is worth up to $288 million, of which the company has received $261.5 million for completing 23 out of 29 progress milestones so far.
    Orbital also hopes to secure the rights to launch commercial, civil and military satellites aboard the Antares. Officials are studying options to build an additional launch base on the west coast.
    Source:Spaceflight Now

    Soyuz rolls out for next South American launch

    The second Soyuz rocket to fly from the commercial launch base in Kourou, French Guiana made a short but meaningful trip on Dec.12, 2011 when it was rolled from the assembly hangar to the pad and rotated to stand up vertically.

    Liftoff is planned for Dec. 16 night at the precise moment of 9:03:08 p.m. EST (11:03 p.m. local time; 0203 GMT) from the Guiana Space Center on the northeastern coast of South America.

    The venerable Russian launcher will head northward to reach a series of sun-synchronous orbits for deployment of three different payloads, initially releasing into a 432-mile circular-orbit the Pleiades 1 high-resolution Earth-imaging spacecraft to be used by the French military, then ejecting a cluster of four electronic eavesdropping spacecraft for France before maneuvering into a 379-mile circular perch to release an Earth observation craft for Chile.

    The three-stage rocket was pieced together inside the hangar constructed at the launch complex, then transported to the pad this morning. The payloads, encapsulated in the rocket's nose cone, will be delivered to the pad and attached to the booster within the protective gantry.

    Source: Spaceflight Now


    Tuesday, December 13, 2011

    Have a close glimpse of Launch Pad 39 A / B in a video

    Pads 39-A and 39-B are virtually identical and roughly octagonal in shape. The distance between pads is 2.6 km. The pad base contains 52,000 cubic meters of concrete. The ramp leading up to the pad is inclined at a 5% grade. The flame trench is 13 meters deep, 137 meters long and 18 meters wide. The orbiter flame deflector is 11.6 meters high, 22 meters long and 17.5 meters wide. It weights 590 t . The SRB deflector is 12.95 meters high, 12.8 meters long and 17.4 meters wide. It weights 499 t. The Sound Suppression Water System is used to protect the launch structure from the intense sound pressure of liftoff. Its water tank is 88.9 meters high and has a capacity of 1,135,000 liters.
    There are 6 permanent and 4 extensible pedestals that are used to support the mobile launch pedestal (MLP) at the pad. Dynamic loads at rebound are 3,175,200 kg  to 4,762,800 kg at liftoff. The pad is lit with 5 clusters of Xenon high-intensity searchlights (total searchlights: 40) around the pad perimeter.

    The height of the Fixed Service Structure (FSS) is 105.7 meters to the top of the lightning mast (referenced to the pad base) and the Rotating Service Structure (RSS) is 57.6 meters high. The Fixed Service Structure (FSS) and Rotating Service Structure (RSS) on Pad 39A underwent a renovation between June and September 1993. Some 13,773 gallons of paint were used on two coats and 1,866 tons of sand were used in the sandblasting operation. 

    Watch the video and have a close glimpse of launch pad systems


    (Courtesy: NASA )

    Launch Acoustics Suppression System at Launch Pad 39A - KSC

     A sound suppression system was installed on the pads and the mobile launcher platform to protect the orbiter and its payloads from being damaged by acoustical energy reflected from the platform during liftoff.

     Image to left: Water is released onto the mobile launcher platform on Launch Pad 39A at the start of a water sound suppression test. Workers and the media (left) are on hand to witness the rare event. This test is being conducted following the replacement of the six main system valves, which had been in place since the beginning of the Shuttle Program and had reached the end of their service life. Also, the hydraulic portion of the valve actuators has been redesigned and simplified to reduce maintenance costs.

    Water stored in a 290-foot-high, 300,000 gallon tank on the northeast side of the pad is released just prior to the main engine ignition and flows by gravity to special outlets on the platform, including six 12-foot-high quench nozzles, or "rainbirds." Nine seconds after liftoff, peak flow rate is 900,000 gallons per minute.

    The system reduces acoustical levels within the orbiter payload bay to about 142 decibels, below the design requirement of 145 decibels.

    Sound Suppression Test Unleashes a Flood
    Birds-eye view of Water Sound Suppression TestA roar resounded from one of the Space Shuttle launch pads May 7 as 350,000 gallons of water rushed across the Mobile Launcher Platform (MLP).

    The torrent of water was released during a test of the water sound suppression system at Kennedy Space Center's Launch Pad 39A.

    Image to left: Water soaks the Mobile Launcher Platform (MLP) on Launch Pad 39A at the peak of a Water Sound Suppression System test. Workers and the media (left) were on hand to witness the rare event. Click image for full size version.

    View of entire launch pad during Water Sound Suppression System test
    Image to right: Huge streams of water cascade down the sides of Launch Pad 39A. Click image for full size version.
    The water system is designed to protect the Shuttle and its payloads from any damage that may occur from acoustical energy reflected from the Mobile Launcher Platform (MLP) during launch. The water is released seconds before ignition of the orbiter's three main engines and twin Solid Rocket Boosters (SRB), then flows through parallel 7-foot-diameter pipes to the Pad.

    The system includes a 290-foot-high water tank filled with 300,000 gallons of water, and it empties in 41 seconds during a launch. Water pours from 16 nozzles on top of the flame deflectors and from outlets in the Shuttle main engine exhaust hole in the MLP at main engine ignition, which occurs approximately 7 seconds before liftoff.

    The system was first installed at the pad when reflective energy from the top of the Mobile Launch Platform was causing minor damage to thermal curtains on the SRBs and putting stress on the wings. After adding the system, the sound pressure was reduced by half.

    Close-up of rainbird nozzleImage to left: This close-up of a "rainbird" -- one of 16 huge nozzles on the Mobile Launcher Platform -- shows the force of the water as it jets across the pad. Click image for full size version.

    The test did more than confirm the six new main system valves performed correctly. Judging from the loud cheers, it also brought even more energy to KSC's Shuttle launch and landing team.

    "It's very exciting for us to do this type of exercise," Payne said. "We had a lot of our folks out here to witness this, and it was a good opportunity to get some training out of it. It was very motivational for us to come out here and do this type of work."

     Watch a Video


     (Courtesy: NASA web Server, You tube)

    Information resouces on cryogenic Engineering


    Links details/descriptions
    Cryogen property programme CATS University of Idaho - cryogen properties database
    Cryogen properties - online An online calculator for thermophysical properties of various gases with graphical or tabular output.
    Cryogenic Data Handbook Selected Cryogenic Data Notebook compiled and edited by J.E. Jensen, W.A. Tuttle, R.B. Stewart, H. Brechna and A.G. Prodell; Brookhaven National Laboratory (BNL 10200-R, Revised August 1980) -- beware the files are up to 10MB large
    Helium T=f(p) International Temperature Scale 1990 - helium vapour pressure temperature equations
    Helium properties Publication: The Observed Properties of Liquid Helium at the Saturated Vapor Pressure by Russell J. Donnelly and Carlo F. Barenghi
    Material property formulas NIST - Cryogenic Technologies Group - material properties formulas


    LinkIntroduction to Cryogenic Engineering

    Link

    Link


     
    Cryogenic Society of America
     
    H2 Incidents and Lessons learnt





    Monday, December 12, 2011

    Report Literature on Liquid / Cryogenic Propellant & Propulsion Systems



    The following is the list of reports available at open sources in pdf format. One can download them freely by clicking on 'View PDF File' link under each titles. However, please note that some of the host servers of the resources (such as NASA Report server) may forbid access when tried from a few selected networks.
    1.  Propulsion Test Handbook: MSFC and SSC
    Online Source: Click to View PDF File [PDF Size: 15.6 MB]
    Publication Year: 2010
    Report/Patent Number: M10-0128
    2. Worldwide Space Launch Vehicles and Their Mainstage Liquid Rocket Propulsion
    Online Source: Click to View PDF File [PDF Size: 3.0 MB]
    Publication Year: 2010
    Report/Patent Number: SPPT-630-0001
    3. Occupational safety considerations with hydrazine fuels
    Online Source: Click to View PDF File [PDF Size: 288 KB]
    Publication Year: 1992
    4. Hypergolic Propellants: The Handling Hazards and Lessons Learned from Use
    Online Source: Click to View PDF File [PDF Size: 56.7 MB]
    Publication Year: 2010
    Report/Patent Number: KSC-2010-045R
    5. Propulsion System Choices and Their Implications
    Online Source: Click to View PDF File [PDF Size: 8.8 MB]
    Publication Year: 2010
    Report/Patent Number: KSC-2010-121
    6. Propellant Mass Fraction Calculation Methodology for Launch Vehicles and Application to Ares Vehicles
    Online Source: Click to View PDF File [PDF Size: 6.0 MB]
    Publication Year: 2009
    Report/Patent Number: M09-0721, M09--0770
    7. Review of Alpha-Ketoglutaric Acid (AKGA) Hydrazine and Monomethylhydrazine (MMH) Neutralizing Compound
    Online Source: Click to View PDF File [PDF Size: 3.1 MB]
    Publication Year: 2009
    Report/Patent Number: NASA/TM-2009-215913, NESC-RP-08-115/08-00474, L-19748, LF99-9325
    8. A Summary of NASA and USAF Hypergolic Propellant Related Spills and Fires
    Online Source: Click to View PDF File [PDF Size: 36.8 MB]
    Publication Year: 2009
    Report/Patent Number: NASA/TP-2009-214769
    9. Safety Standard for Hydrogen and Hydrogen Systems: Guidelines for Hydrogen System Design, Materials Selection, Operations, Storage and Transportation
    Online Source: Click to View PDF File [PDF Size: 13.9 MB]
    Publication Year: 1997
    Report/Patent Number: NASA-TM-112540, NAS 1.15:112540, NSS-1740.16-Rev
    10. Hypergol Systems: Design, Buildup, and Operation
    Online Source: Click to View PDF File [PDF Size: 9.9 MB]
    Publication Year: 2006
    11. Zero-Boil-Off Liquid Hydrogen Storage Tanks
    Online Source: Click to View PDF File [PDF Size: 1.2 MB]
    Publication Year: 2009
    12. LOX Tank Helium Removal for Propellant Scavenging
    Online Source: Click to View PDF File [PDF Size: 4.8 MB]
    Publication Year: 2009
    Report/Patent Number: E-17143-V
    13. Spray-On Foam Insulations for Launch Vehicle Cryogenic Tanks
    Online Source: Click to View PDF File [PDF Size: 9.6 MB]
    Publication Year: 2011
    Report/Patent Number: KSC-2011-140
    14. Cryogenic Vacuum Insulation for Vessels and Piping
    Online Source: Click to View PDF File [PDF Size: 2.6 MB]
    Publication Year: 2010
    Report/Patent Number: KSC-2010-126
    15. Cryogenic Moisture Apparatus
    Online Source: Click to View PDF File [PDF Size: 1.6 MB]
     http://www.techbriefs.com/component/content/article/7931
    Publication Year: 2010
    Report/Patent Number: KSC-13049
    16. Measurement of Insulation Compaction in the Cryogenic Fuel Tanks at Kennedy Space Center by Fast/Thermal Neutron Techniques
    Online Source: Click to View PDF File [PDF Size: 49 KB]
    Publication Year: 2010
    Report/Patent Number: KSC-2010-273
    17. Thermographic Methods of Detecting Insulation Voids in Large Cryogenic Tanks
    Online Source: Click to View PDF File [PDF Size: 27 KB]
    Publication Year: 2010
    Report/Patent Number: KSC-2010-243
    18. Gauging Systems Monitor Cryogenic Liquids
    Online Source: Click to View PDF File [PDF Size: 146 KB]
    Publication Year: 2009
    Document ID: 20090039421
    19. Expandable Purge Chambers Would Protect Cryogenic Fittings
    Online Source: Click to View PDF File [PDF Size: 535 KB]http://www.techbriefs.com/index.php?option=com_staticxt&staticfile=/Briefs/Feb04/KSC12460.html
    Publication Year: 2004
    Report/Patent Number: KSC-12460
    20. Thermal Performance of Cryogenic Piping Multilayer Insulation in Actual Field Installations
    Online Source: Click to View PDF File [PDF Size: 240 KB]
    Publication Year: 2002
    Document ID: 20020039045

    Report Literature on Launch Pads ...

    The following is the list of reports available at open sources in pdf format. One can download them freely by clicking on 'View PDF File' link under each titles. However, please note that some of the host servers of the resources (such as NASA Report server) may forbid access when tried from a few selected networks.

    1. Launch Pad Escape System Design (Human Spaceflight)
    Online Source: Click to View PDF File [PDF Size: 2.5 MB]
    Report/Patent Number: KSC-2011-096
    2. Adhesion Testing of Firebricks from Launch Pad 39A Flame Trench after STS-124
    Online Source: Click to View PDF File [PDF Size: 14.8 MB]
    Report/Patent Number: NASA/TM-2009-214759
    3. Lightning Strike Sensing System for the Space Shuttle Launch Pad
    Online Source: Click to View PDF File [PDF Size: 84 KB]
    Report/Patent Number: AD-A525052
    4. Rocket Noise and Vibration Shuttle/Payload Processing and ISS: Launch Pad Vibroacoustics Research at NASA/KSC
    Online Source: Click to View PDF File [PDF Size: 3.7 MB]
    Report/Patent Number: KSC-2002-131
    5. Lightning Threat Analysis for the Space Shuttle Launch Pad and the Payload Changeout Room Using Finite Difference Methods
    Online Source: Click to View PDF File [PDF Size: 2.4 MB]
    Report/Patent Number: NASA-CR-205186, NAS 1.26:205186, EMA-97-010
    6. Launch Pad Lightning Protection Enhancement by Induced Streamers
    Online Source: Click to View PDF File [PDF Size: 5.6 MB]
    Accession Number: 93N24876
    7. Effect of 25 cycles of launch pad exposure and simulated mission heating on space shuttle reusable surface insulation
    coated with reaction cured glass

    Online Source: Click to View PDF File [PDF Size: 5.4 MB]
    Report/Patent Number: NASA-TM-80160
    Updated/Added to NTRS: Mar 16, 2009
    8. Launch pad to the moon: Construction bidding cost of Launch Complex 39, part 1
    Online Source: Click to View PDF File [PDF Size: 286 KB]
    Report/Patent Number: NASA-TM-109269, NAS 1.15:109269
    9. KSC VAB Aeroacoustic Hazard Assessment
    Online Source: Click to View PDF File [PDF Size: 9.4 MB]
    Publication Year: 2010
    Report/Patent Number: KSC-2010-112
    10. Rocket Noise and Vibration Shuttle/Payload Processing and ISS: Launch Pad Vibroacoustics Research at NASA/KSC
    Online Source: Click to View PDF File [PDF Size: 3.7 MB]
    Report/Patent Number: KSC-2002-131

    Some more ebook titles ...

    Pl. do not download as they are Copy Righted. Pl browse through. If  found useful, pl check whether your library already has them. If  not, pl. indent for the same.

    Spacecraft Reliability and Multi-state Failures (by Joseph Homer  Saleh)
    * provides new nonparametric results pertaining to spacecraft reliability based on extensive statistical analysis of on-orbit anomaly and failure data;
    * develops parametric models of spacecraft and spacecraft subsystem reliability and multi-state failures
    * quantifies the relative contribution of each subsystem to the failure of the satellites
    * proposes advanced stochastic modeling and analysis tools for the reliability and survivability of spacecraft and space-based networks.
    * provides a dedicated treatment of the reliability and subsystem anomalies of communication spacecraft in geostationary orbit.        Link


     

    Satellite Communications - Ground Segment and Earth Station Handbook
    From international telephone network gateways to direct broadcast home receivers, today’s broad range of ground systems and devices require satellite communication engineers and business managers to have a broad and sound understanding of the design and operating principles of earth stations and ground control facilities. This volume offers an exploration of the delivery end of the satellite link and its relationship to the delivery of services.  Link





    Satellite Orbits: Models, Methods and Applications, by Oliver Montenbruck
    This is a modern textbook that guides the reader through the theory and practice of satellite orbit prediction and determination. Starting from the basic principles of orbital mechanics, it covers elaborate force models as well as precise methods of satellite tracking. Emphasis is on numerical treatment and a multitude of algorithms adopted in modern satellite trajectory computation are described in detail. The book addresses students, scientist working in the field of navigation, geodesy and spaceflight technology and satellite engineers and operators focusing on spaceflight dynamics.    Link



     Spacecraft Power Technologies, by Anthony K.Hyder
    While there are numerous books and other literature on spacecraft electrical power systems, there are no comprehensive single references describing the enabling technologies used in spacecraft power systems. This book fills that need. Rather than describing specific power systems used in various space flights, Spacecraft Power Technologies details three of the most commonly used types of energy sources used in spacecraft power systems—solar, chemical, and nuclear sources. Link




    Spacecraft Systems Engineering, by Peter Fortescue
    This fourth edition of the bestselling Spacecraft Systems Engineering title provides the reader with comprehensive coverage of the design of spacecraft and the implementation of space missions, across a wide spectrum of space applications and space science. The text has been thoroughly revised and updated, with each chapter authored by a recognized expert in the field.  Three chapters – Ground Segment, Product Assurance and Spacecraft System Engineering – have been rewritten, and the topic of Assembly, Integration and Verification has been introduced as a new chapter, filling a gap in previous editions. Link