Newgrounds

Users cannot link directly to a page with the flash file without the interstitial launch page. Unlike the shuttle, this future launcher and associated crew exploration vehicle will have a launch escape system to save the crew in the event of a disaster. Clicking this button spawns a pop-up window showing the flash file. This contrasts with the current shuttle where astronauts and heavy cargo are launched in a single vehicle. Linking to an item on Newgrounds can only be made to a launch page, where the reader has to find and click on a Watch this movie button. This technology would be used to develop two separate launchers, one for manned missions and the other for unmanned heavy cargo. These could be blocked using the browser or add-on software, except that to use the site, users would have to configure an exception for Newgrounds, exposing them to the advertising. NASA plans on using modified shuttle components to build an expendable Shuttle Derived Launch Vehicle.

Newgrounds uses pop-up advertising. NASA currently uses these for unmanned launches, and plans to use them for future manned launches. Around 2004, people began to complain that Newgrounds.com had been adding spyware, such as 180 Solutions to certain webpages. Another approach is lower cost expendable launch vehicles. Astroseries 2 became the very first submission to be received by Newgrounds in 2006. Like the X-33, the X-30 encountered major technical difficulties, primarily due to the system complexity and materials required for hypersonic flight, and was finally cancelled. None have been made since spring of 2005, and it's unlikely that more will be made. The official name was the Rockwell X-30.

These collections have no theme, and seem to be primarily compilations of rejected or unused daily collection animations. Department of Defense, but passenger-carrying civilian versions were planned, sometimes called the "New Orient Express". Some daily collections were submitted simply under the name "DailyToon________" with the cartoon's submission date in the blank space. It was originally investigated by the U.S. Certain collections are based after people, while others have been based on movies, cartoon characters, and video games. It would achieve much of orbital velocity while still within the upper atmosphere. Most of them are based on TV shows, mainly sitcoms, anime productions, and kids' shows. This would be launched and landed horizontally like an airliner.

The daily collections are generally themed. Another variant of SSTO is a hypersonic, scramjet-powered, airbreathing vehicle. As such, various other "Clocks" have guested on daily collections, as well as members of the similar "Star Syndicate", who also produce their own type of daily cartoons. During design that program increased in complexity and development cost, encountered problems and was finally cancelled. These collections are masterminded by Newgrounds user "Coolboyman", better known as "Strawberry Clock", the self proclaimed "King of the Newgrounds Portal" and leader of the infamous Clock Crew. NASA evaluated several concepts in the 1990s, and selected the X-33, which would eventually have been the Venturestar. Each collection features from four to five animations, typically with each cartoon produced by a single animator. One approach is Single Stage To Orbit (SSTO), which would be 100% reusable and use a single stage.

Due to the short timeframe, the majority of the included animations are of poor quality, featuring little (if any) animation and for the most part, speech to voice synthesis used for voices. In general future designers look to less complex, more reliable launch systems with lower maintenance costs. They were written, created, and submitted to Newgrounds within the course of one day. Nixon in 1971 [4], the operational costs, flight rate, payload capacity, and reliability have been worse than anticipated. Daily collections are existed between 2004 and 2005. While it was developed within the original development cost and time estimates given to President Richard M. Currently there are a lot of collaborations based on songs, with each participating author animating one or more line each, because of the huge amount of collabs being started at the same time and spamming the Newgrounds Flash forum some members took it upon themselves to create the website NGCollabs where people with a batting average (average score of their Flash submissions) of lower than 3.00 could start collaborations. Opinions differ on the lessons of the Shuttle.

They are also a great way for up-and-coming artists to get in the spotlight with the bigshots. Advances in technology over the last decade have made probes smaller and lighter, and as a result unmanned probes and communications satellites can use relatively cheap and reliable expendable rockets, including Delta launcher, and Atlas V. Collaborations are a great way for artists to work together and get to know each other. The Shuttle's history of unexpected delays also makes it liable to miss the narrow launch windows. It began with group works by the Clock Crew and flourished when the Newgrounds Time Trials sparked a more general interest among authors. Following the Challenger disaster, carrying in the shuttle payload bay the powerful liquid fueled Centaur upper stages planed for interplanetary probes was ruled out. Another popular activity on Newgrounds is the collab—various animators, artists and programmers collaborating on a single movie or game. NASA's plan for using the shuttle to launch all unmanned payloads declined, then was discontinued.

Various flash series submitted exclusively to Newgrounds. No other launch vehicle had the shuttle's payload capability or could return large items from the space station to earth. His work includes:. Even though the initially planned Space Station Freedom was signficantly scaled back, the shuttle was still vital to service it. These are referred to as Newgrounds Originals. During development, shuttle features were primarily chosen based on capability required to service the future space station. Tom Fulp has submitted several movies and games to Newgrounds. The result is high labor cost, with around 25,000 workers in Shuttle operations and labor costs of about $1 billon per year.

The NG chat has spawned many spinoffs, such as #radiogrounds (The radiogrounds.com chat), #ngdrunks for the NGDr0kns (dr0kn.com), #blamclub for the blamclub (ADG/BlamClub Forums) and many other (smaller) user-made channels such as #ngpoker for the NG Late Night Poker Club, #nazigrounds.com, and #minimanjapan.com (minimanjapan.com). Furthermore, because in some cases there are no survivable abort modes, many pieces of hardware simply must function perfectly and so must be carefully inspected before each flight. The NG Chat is accessible via any IRC client by entering the java.webchat.org, area.webchat.org or irc.webmaster.com servers and joining the channel through the irc command: /join #newgrounds.com. Because loss of crew is unacceptable, the primary focus of the Shuttle program is to return the crew to Earth safely, which can conflict with other goals, namely to launch payloads cheaply. You go in, you get insulted and insult back. Instead, this turnaround process usually takes months, however once Columbia was launched twice within 56 days. The Insult room is somewhat self-explanatory. After landing, the orbiter would be checked out and start "mating" to the rest of the system (the ET and SRBs), and be ready for launch in as little as two weeks.

The Hookup room is for any users who wish to "Chat intimately", trade pictures of one another, etc., to deter users from doing so in the main chat. The Shuttle was originally conceived to operate somewhat like an airliner. NG Chat also has two other smaller, less frequented channels: the Hookup room (#nglove) and the Insult room (#ngwar). Some reasons for higher than expected operational costs can be ascribed to:. If an AOL user enters the NG Chat, they are automatically kicked upon entry. Another way to calculate launch cost is the incremental expense of adding a single additional shuttle mission, which is is about $100 million. America Online (AOL) users on Java clients are not allowed into the NG Chat, because their IP Mask changes dynamically when the user begins a new dial-up session, so bans and akicks can't directly affect one person using that ISP (in any geographical region). Some of this can be attributed to operating beyond the 10-year anticipated lifespan of each Shuttle, and higher than anticipated maintenance costs.

Many people join and chat about whatever they deem fit. This has been much more expensive than anticipated. It's accessible via the CHAT button on the navigation bar at Newgrounds.com, or via any IRC client, such as mIRC, IRCle, Firefox's IRC clients, Trillian, etc. This includes all related costs such as maintenance, ground facilities, training, etc., and divides that figure by the number of shuttle flights. Newgrounds has its own chat, usually referred to as the NG Chat. There are various ways to calculate costs -- the $500 million figure inclues all operational details of maintaining and servicing the Shuttle fleet. The forums for regular members consist of the General section, the Politics section, the Programming section, the Flash section, the Clubs & Crews section, the Where Is/How To? section, the NG News section (for any and all news posts made by admins), the Network News section (For anything pertaining to the tech aspects of the BBS), the P-Bot's Posts section (for Portal updates from the automated Portal Bot, aka P-Bot), and the recently added Audio forum. Per launch costs are roughly $500 million today.

Next to the Flash Portal, the BBS seems to be the most popular part of the site. However, this does not fully explain the high shuttle operational costs. Site administrator, Wade Fulp, also clears the BBS of spam by deleting accounts that violate rules, a process which he calls 'terminating' or 'axing'. Nixon in 1971 [3]. Thanks to the moderators, it is kept relatively free of spam. In fact when discounting inflation, the shuttle development program was within the initial cost estimate given to President Richard M. Other forums are private, for use by moderators. When evaluating shuttle development costs in later-year dollars, this superficially appeared to be a large cost overrun in the program.

Some are reply-only, where you can't start a new topic, but are welcome to read and reply to existing topics. Between when the program began in 1972, and first flight in 1982, inflation increased prices over 200%. Some are all access, where all users are welcome to read, post and reply. suffered from severe inflation. The BBS (Bulletin Board System) is a very popular forum on the site, which consists of multiple forums. During the 1970s the U.S.
. One reason behind this apparent failure is inflation.

Note: You must have at least 30 reviews that week to win an award that involves calculating the review score as well, such as the Underdog or Review Crew Pick awards. Although the final design differs from the original concept, the project was still supposed to meet USAF goals and be much cheaper to fly in general. When a movie or game is submitted to the Flash Portal, it has the chance to win any of the following awards:. Although it did operate as the world's first reusable crew-carrying spacecraft, it did not improve on those parameters in any meaningful way, and is considered by some to have failed in its original purpose. . It was intended to improve greatly on the previous generation of single-use manned and unmanned vehicles.
. The original mission of the Shuttle was to operate at a high flight rate, at low cost, and with high reliability.

On July 6, 2005, Newgrounds celebrated its ten year anniversary. [2]. The site now has over 900,000 registered members and over 291,000 submissions. NASA's budget for 2005 allocates 30%, or $5 billion, to Space Shuttle operations. This system of public voting creates a sense of community in Newgrounds and keeps visitors coming back for more. The total cost of the program has been $145 billion as of early 2005 ($112 billion of which was incurred while the program was operational) and is estimated at $174 billion when the Shuttle retires in 2010. A user-friendly system of voting and rating produces lists that directs visitors to the most popular flash movies and allows the Newgrounds site designers to easily locate any material that might be considered for deletion or promotion. While the Shuttle has been a reasonably successful launch vehicle, it has been unable to meet its goal of radically reducing flight launch costs, as the average launch expenditures during its operations up to 2005 accumulates to $1.3 billion [1], a rather large figure compared to the initial projections of $10 to $20 million.

Visitors are encouraged to review the various submissions that they encounter on the site, as a means of providing other potential visitors with a vague idea of what they can expect from the many flash movies and games to choose from. The Columbia Accident Investigation Board called this tendency the "normalization of deviance" -- a gradual acceptance of abnormal events simply because they haven't been catastrophic to date. Over the years Newgrounds has grown to an incredible size, and with so much material to offer, it must rely on the willing cooperation and support of its many visitors in order to function properly. Over time NASA managers gradually accepted more tile damage, similar to how O-ring damage was accepted. This site allows its users to submit their own Flash movies, games, and music, and view submissions from other users. The original shuttle operational specification said the orbiter thermal protection tiles were designed to withstand virtually no debris hits at all. Tim, Tom's former roommate, also assists in running the site. The foam had not been designed or expected to break off, but had been observed in the past to do so without incident.

It was created and is currently owned by Tom Fulp, who is assisted by his brother Wade Fulp, and is also helped by liljim, an administrator living in England. Columbia failed because of damaged thermal protection from foam debris that broke off the external tank during ascent. Newgrounds is a website that hosts Macromedia Flash animations and games. Challenger's O-ring eroded completely through, with fatal results. Ben Edelman on 180 Solutions. Unfortunately NASA and Thiokol senior managers overruled him and allowed the launch to proceed. "Newgrounds and Me". He raised concerns that the unusually cold temperatures would stiffen the O-rings, preventing a complete seal.

"180 Solutions: Kill The Sleaze Ads". Morton Thiokol designed and manufactured the SRBs, and during a pre-launch conference call with NASA, the Thiokol engineer most experienced with the O-rings pleaded repeatedly to cancel or reschedule the launch. Shroud. Instead of finding out why, managers felt because it had not previously eroded by more than 30%, that this was not a hazard as there was "a factor of three safety margin". Dr. In the case of Challenger, an O-ring which should not have eroded at all did, in fact, erode on earlier shuttle launches. Burnt Face Man. In both cases a mind set among senior managers developed that concerns had to be objectively proven rather than simply suspected.

Madness Combat. A heavily layered, procedure-oriented bureaucratic structure inhibited necessary communication and action. Miss Dynamite. In both cases the vehicle gave ample warning beforehand of abnormal problems. YAAFM. In both cases, junior engineers were greatly concerned about possible problems, but these concerns were not properly communicated to or understood by senior NASA managers. Retarded Animal Babies. In both cases events happened which were not planned for or anticipated.

Waterman. While the technical details of the accidents are quite different, the organizational problems show remarkable similarities. College University. This gives a 2% death rate per astronaut per flight. Salad Fingers. Two Shuttles have been destroyed in 114 missions, both with the loss of the entire crew of seven:. Neurotically Yours. † Satellites deployed
* This was flight STS-80, during November 1996.

Broken Saints. Whilst all three Orbiters are externally very similar, they have minor internal differences; new equipment is fitted on a rotating basis as they are maintained, and the newer Orbiters tend to be structurally lighter. Xombie. Individual Orbiters are both named, in a manner similar to ships, and numbered, using the NASA Orbiter Vehicle Designation system. Pico's School. After landing the vehicle stands on the runway to permit the poisonous hydrazine fumes used for part of the attitude control during descent to dissipate. House Hunting. Landing speed is very high -- 213 to 255 mph, vs 160 mph for a jet airliner.

Harry Pothead. It glides to landing with a glide angle of 4:1. Domo Kun Angry Smash Fest!. In the lower atmosphere the orbiter flies much like a conventional glider, except for a much higher descent rate, over 10,000 feet per minute (roughly 20 times that of an airliner). Dad 'n Me. Attitude control is achieved from a mixture of RCS thrusters and control surfaces. Club-A-Seal. This is achieved by performing s-curves at up to 70 degree bank angle.

Beep-Me Jesus. In addition, the standard reentry aims deliberately high- the vehicle needs to bleed off extra altitude and speed to reach the landing site. Alien Hominid (Later remade for PlayStation 2, Nintendo GameCube (US only), Xbox (Europe only) and Game Boy Advance.). The vehicle attitude is controlled to take on a nose up attitude of up 40 degrees to maximise drag. Turd of the Week: (Frequently referred to as TOTW) It is given to the submission with the lowest score that manages to pass judgement. The vehicle will then start significantly entering the atmosphere at about 400,000 ft doing around Mach 25. Underdog of the Week: (Often referred to as UOTW) This award is given to the submission with the biggest discrepancy between the review score and the popular vote. However the reentry can be and has (once) been flown manually.

Review Crew Pick: This award is given to the submission with the best "overall" score in reviews. The entire reentry, except for the lowering of the undercarriage, is under complete computer control. Weekly 2nd/3rd/4th/5th Place: Lesser awards given to submissions each week. This OMS firing is done roughly halfway around the globe from the landing site. Weekly Users Choice: The award given to the submission that scored the highest for the week. The deceleration of the Shuttle lowers its orbit perigee down into the atmosphere. Daily 2nd/3rd/4th/5th Place: Lesser awards given to submissions each day. The vehicle begins reentry by firing the OMS engines in the opposite direction to the orbital motion for about three minutes.

Daily Feature: The award given to the submission that scored the highest for the day. The Shuttle then fires the OMS engines to circularize the orbit and avoid reentry. At this point the Shuttle is still slightly suborbital, since the trajectory intersects the atmosphere. The tank then falls to largely burn up in the atmosphere, with some fragments falling into the Indian Ocean. Before complete depletion of propellant (running dry would destroy the engines) the main engines are shutdown, and the empty external tank is released by firing explosive bolts.

Finally, in the last tens of seconds of the main engine burn, the mass of the vehicle is low enough that the engines must be throttled back to limit vehicle acceleration to 3g, largely for astronaut health and comfort. The vehicle continues to climb and takes on a somewhat nose-up angle to the horizon — it uses the main engines to gain and then maintain altitude whilst it accelerates horizontally towards orbit. However, as the burn continues, the weight of the propellant reduces, the ever-lighter vehicle produces more and more acceleration until the thrust to weight ratio exceeds 1 again and the vehicle can hold itself up. The vehicle at that point in the flight has a thrust to weight ratio of less than one — the main engines actually have insufficient thrust to exceed the force of gravity, and the vertical speed given to it by the SRBs temporarily decreases.

The Shuttle then begins accelerating to orbit on the Space Shuttle Main Engines. The SRBs parachute back to the ocean to be reused. 126 seconds after launch, explosive bolts release the SRBs and small separation rockets push them laterally away from the vehicle. Around a point called "max-q", where the aerodynamic forces are at their maximum, the main engines are temporarily throttled back to avoid overspeeding and hence overstressing the Shuttle (particularly vulnerable parts such as the wings).

Orbital velocity at the 380 km (236 miles) altitude of the International Space Station is 7.68 km per second, or 17,180 mph, roughly equivalent to Mach 23. This isn't visually obvious since the vehicle rises vertically and is out of sight for most of the horizontal acceleration. To achieve orbit requires expending much more energy in a horizontal direction than in a vertical direction. The vehicle climbs in a progressively flattening arc, accelerating as the weight of the SRBs and main tank decrease.

Shortly after clearing the tower the Shuttle rotates so that the vehicle is below the external tank and SRBs. At takeoff the vast majority (~71%) of the thrust is provided by the SRBs. After the Challenger disaster, there were extensive upgrades to abort modes. Many of these concern SSME failures, since that is the most complex and highly stressed component.

There are extensive emergency procedures (abort modes) to handle various failure scenarios during ascent. The SRBs cannot be turned off once ignited, and afterwards the shuttle must take off, no matter what. Initially the main engines are ignited and computers verify their operation for several seconds; if successful, the SRBs are ignited and the vehicle is then committed to takeoff. It is called the Shuttle-C and would trade re-usability for cargo capability with large potential savings from reusing technology developed for the Space Shuttle.

A cargo-only, unmanned variant of the Shuttle has been variously proposed and rejected since the 1980s. In addition the Air Force developed their own much lighter single-piece SRB design using a filament-wound system, but this too was cancelled. The loss of the ASRB program forced the development of the Super LightWeight external Tank (SLWT), which provides some of the increased payload capability, while not providing any of the safety improvements. These culminated in the considerably simpler, lower cost, probably safer and better performing Advanced Solid Rocket Booster which was to have entered production in the early to mid-1990s to support the Space Station, but was later cancelled to save money after the expenditure of $2.2 billion.

Several other SRB improvements were planned in order to improve performance and safety, but never came to be. Notable is the adding of a third O-ring seal to the joints between the segments, which occurred after the Challenger accident. The SRBs (Solid Rocket Boosters) have undergone improvements as well. As the Shuttle cannot fly unmanned, each of these improvements has been "tested" on operational flights.

It weighs 7,500 lb (3.4 t) less than the last run of lightweight tanks. This version of the tank is made of the 2195 Aluminum-Lithium alloy. STS-91 saw the first flight of the "super light-weight external tank". The resulting "light-weight external tank" has been used on the vast majority of Shuttle missions.

Additional weight was saved by removing some of the internal "stringers" in the hydrogen tank that proved unnecessary. The 600lbs saved by not painting the tank results in an almost 600lb increase in payload capability to orbit. For STS-1 and STS-2 the external tank was painted white to protect the insulation that covers much of the tank, but improvements and testing showed that it was not required. The normal maximum throttle is 104%, with 106% and 109% available for abort emergencies.

The 109% thrust level was finally reached in flight hardware with the Block II engines in 2001. The upgrades have improved engine reliability, maintainability and performance. SSME upgrades are denoted as "block numbers", such as block I, block II, and block IIA. However this would have required revising much previous documentation and software, so the 104% number was retained.

They could have rescaled the output number, saying in essence 104% is now 100%. During the lengthy development program, Rocketdyne determined the engine was capable of safe reliable operation at 104% of the originally specified thrust. The 100% figure is the original specified power level. This explains phrases such as "Main engines throttling up to 104%." This does not mean the engines are being run over a safe limit.

The Space Shuttle Main Engines have had several improvements to enhance reliability and power. With the coming of the Space Station, the Orbiter's internal airlocks are being replaced with external docking systems to allow for a greater amount of cargo to be stored on the Shuttle's mid-deck during Station resupply missions. In the Apollo-Soyuz Test Project tradition, programmable calculators are carried as well (originally the HP-41C). This is called a "glass cockpit".

In addition to the computer upgrades, the original vector graphics monochrome cockpit displays were replaced with modern raster color displays, similar to contemporary airliners like the Airbus A320. Internally the Shuttle remains largely similar to the original design, with the exception of the improved avionics computers. The memory was changed from magnetic core to semiconductor with battery backup. In 1990 the original computers were replaced with an upgraded model AP-101S, which has about 2.5 times the memory capacity (about 1 megabyte) and three times the processor speed (about 1.2 million instructions per second).

They have no hard disk drive, but load software from tape cartridges. The CPU could process about 400,000 instructions per second. The IBM AP-101 computers originally had about 424 kilobytes of magnetic core memory each. It is specifically designed for a real time embedded system environment.

The software for the shuttle computers are written in a high-level language called HAL/S, somewhat similar to PL/I. However in theory it can fail, so the BFS exists for that contingency. For example the number of code lines is tiny relative to a commercial operating system, changes are only made infrequently and with extensive testing, and many programming and test personnel work on the small amount of computer code. This should never happen, as embedded system avionic software is developed under totally different conditions than commercial software.

The BFS was created because although the four primary computers are hardware redundant, they all run the same software, so a generic software problem could crash all of them. The Backup Flight System (BFS) is separately developed software running on the fifth computer, used only if the entire four-computer primary system fails. In the rare case of two out of four computers simultaneously failing (a two-two split), one group is picked at random. If a second computer of the three remaining fails, the two functioning computers vote it out.

This isolates it from vehicle control. If one computer fails the three functioning computers "vote" it out of the system. The four general purpose computers operate essentially in lockstep, checking each other. After two failures it can land safely.

After a single failure the shuttle can continue the mission. The design goal of the shuttle DPS is fail operational/fail safe reliability. Collectively they are called the shuttle Data Processing System (DPS). A fifth backup computer runs separate software called the Backup Flight System (BFS).

Four computers run specialized software called the Primary Avionics Software System (PASS). The shuttle uses five identical redundant IBM 32-bit general purpose computers (GPCs), model AP-101, constituting a type of embedded system. Much research went into the shuttle computer system. A primary concern with digital fly-by-wire systems is reliability.

This means no mechanical or hydraulic linkages connect the pilot's control stick to the control surfaces or reaction control system thrusters. The shuttle was one of the earliest aircraft to use a computerized fly-by-wire digital flight control system. The SRB cases are made of steel about 1/2 inch (1.27 cm) thick. They are jettisoned two minutes after launch at a height of 36 nautical miles (67 km), then deploy parachutes and land in the ocean to be recovered.

The Solid Rocket Boosters (SRBs) contain the solid fuel that provides about 71% of the vehicle's liftoff thrust. The ET is made of aluminum-lithium alloy. It is discarded 8.5 minutes after launch at an altitude of 60 nautical miles (111 km) then burns up on reentry. The External Tank (ET) contains the 2 million liters (528,000 gallons) of liquid hydrogen and liquid oxygen propellant that feeds the SSMEs.

The orbiter structure is made primarily from aluminum alloy, although the engine thrust structure is made from titanium. Unlike previous space vehicles which used insulation that burned off during reentry and couldn't be reused, the orbiter thermal protection can be reused up to 100 times with only minor repairs. Lower temperature areas on the upper surfaces are protected by flexible thermal blankets. The underbelly and much of the fuselage sides is protected by silica tiles.

The hottest areas are on the wing leading edges and nose, which are protected by reinforced carbon/carbon. Various materials are used, depending on the amount of heat. The Thermal Protection System (TPS) covers the outside of the obiter, protecting it from the intense heat during reentry. The Reaction Control System (RCS) provides attitude control and translation along the pitch, roll, and yaw axes during the flight phases of orbit insertion, orbit, and reentry.

The Orbital Maneuvering System (OMS) provides orbital maneuvers, including insertion, circularization, transfer, rendezvous, abort to orbit, and abort once around. They are used for propulsion during ascent. Three Space Shuttle Main Engines (SSMEs) are mounted in the rear part of the obiter. Since the arm is a crucial part of the Thermal Protection Inspection procedures now required for Shuttle flights, it will probably be included on all future flights.

Until the loss of Columbia, the Canadarm had been used only on those missions where it was needed. Inside the payload bay is the Remote Manipulator System, also known as the Canadarm, a robot arm used to retrieve and deploy payloads. Thermal control is also maintained by adjusting the orientation of the Shuttle relative to Earth and Sun. The payload bay doors have heat radiators mounted on their inner surfaces, and so are kept open for thermal control while the Shuttle is in orbit.

The orbiter has a large 60 by 15 ft (18  m by 4.6 m) payload bay, filling most of the fuselage. Astronauts pass through the airlock hatch to put on their space suits. Galley, toilet, sleep locations, storage lockers, and the side hatch for entering/exiting the vehicle is also located there, as is the airlock hatch into the payload bay. The mid-deck has three more seats for the rest of the crew members.

The highest flight deck seats the commander and pilot, two mission specialists in the back. Its crew cabin consists of three levels: the flight deck, the mid-deck, and the utility area. The orbiter resembles an airplane with delta wings. The vehicle is launched vertically like a conventional rocket, and the orbiter glides to a horizontal landing like an airplane, after which it is refurbished for reuse.

The tank and boosters are jettisoned during ascent, so only the orbiter goes into orbit. The shuttle is a partially reusuable launch system composed of three main assemblies: the reusable Orbiter Vehicle (OV), the expendable External Tank (ET), and the two reusable Solid Rocket Boosters (SRBs). Columbia was lost, with all seven crew members, during reentry on February 1, 2003, and has not been replaced. Endeavour was built to replace it (using spare parts originally intended for the other Orbiters) and delivered in May 1991.

Challenger was destroyed when she disintegrated during launch on January 28, 1986, with the loss of all seven astronauts on board. The Shuttle was meant to visit Space Station Freedom, announced in 1984, an ambitious and much-delayed project later downsized and merged into the International Space Station program. Challenger was delivered to KSC in July 1982, Discovery was delivered in November 1983, and Atlantis was delivered in April 1985. The first fully functional Shuttle Orbiter, built in Palmdale, California, was the Columbia, which was delivered to Kennedy Space Center on March 25, 1979, and was first launched on April 12, 1981—the 20th anniversary of Yuri Gagarin's space flight—with a crew of two.

Amid great fanfare, the Enterprise was rolled out on September 17, 1976, and later conducted a successful series of glide-approach and landing tests that were the first real validation of the design. The first complete Orbiter was originally named Constitution, but a massive write-in campaign from fans of the Star Trek television series convinced the White House to change the name to Enterprise. The contractor for the Space Shuttle Solid Rocket Boosters was Morton Thiokol (now part of Alliant Techsystems), for the external tank, Martin Marietta (now Lockheed Martin), and for the Space shuttle main engines, Rocketdyne. The prime contractor for the program was North American Aviation (later Rockwell International), the same company responsible for the Apollo Command/Service Module.

The final design was less costly and less technically ambitious than earlier fully reusable designs. The Shuttle program was formally launched on January 5, 1972, when President Nixon announced that NASA would proceed with the development of a reusable Space Shuttle system. Ultimately the current design was chosen, using a reusable winged orbiter, solid rocket boosters, and expendable external tank. During early shuttle development there was great debate about the optimal shuttle design that best balanced capability, development cost and operating cost.

They evaluated the shuttle studies to date, and recommended a national space strategy including building a space shuttle. Agnew. Nixon formed the Space Task Group, chaired by vice president Spiro T. In 1969 President Richard M.

The early studies were denoted "Phase A", and in June 1970, "Phase B", which were more detailed and specific. Even before the Apollo moon landing in 1969, in October 1968 NASA began early studies of space shuttle designs. .
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However, following the STS-114 return-to-flight mission in August 2005, the Shuttle program is currently grounded pending repairs and the solution of outstanding safety issues. According to the Vision for Space Exploration, use of the Space Shuttle will be focused on completing assembly of the ISS in 2010, after which it will be replaced by the yet-to-be-developed Crew Exploration Vehicle (CEV). The program started in the late 1960s and has dominated NASA's manned operations since the mid-1970s. Each Shuttle was designed for a projected lifespan of 100 launches or 10-years operational life.

However this cabability is used to return large payloads to earth from the International Space Station, as the Russian Soyuz has limited capacity for return payloads. While the vehicle was designed with the capability to recover satellites and other payloads from orbit and return them to Earth, this capacity has not been used often. It carries large payloads to various orbits, provides crew rotation for the International Space Station (ISS), and performs servicing missions. It is also the first winged manned spacecraft to achieve orbit and land.

The Shuttle is the first orbital spacecraft designed for partial reusability. When its mission is complete, it re-enters the earth's atmosphere and makes an unpowered gliding horizontal landing, usually on a runway at Kennedy Space Center. The winged shuttle orbiter is launched vertically, carrying usually five to seven astronauts and up to about 22,700 kg (50,000 lbs) of payload into low earth orbit. NASA's Space Shuttle, officially called Space Transportation System (STS), is the United States government's sole manned launch vehicle currently in service.

The trailer allows the transportation of the Orbiter from the OPF to either the SCA-747 "Mate-Demate" stand or the VAB without placing any additional stress on the undercarriage. Prior to the closing of the Vandenburg facility, Orbiters were transported from the OPF to the VAB on its undercarriage, only to be raised when the Orbiter was being lifted for attachment to the SRB/ET stack. Air Force's launch facility at Vandenburg Air Force Base in California (since then converted for Delta V rockets) that would transport the Orbiter from the landing facility to the launch pad, which allowed both "stacking" and launch without utilizing a separate VAB-style building and crawler-transporter roadway. A 36-wheeled transport trailer, originally built for the U.S.

The Shuttle Carrier Aircraft is a modified Boeing 747 that flies the Space Shuttle from alternative landing sites back to Cape Canaveral. The Crawler-Transporter moves the Space Shuttle from the Vehicle Assembly Building to Launch Complex 39. While the shuttle might safely endure a lightning strike, a similar strike caused problems on Apollo 14, so for improved safety NASA chooses to not launch the shuttle if lightning is possible. However upon takeoff the shuttle sends out a long exhaust plume as it ascends, and this plume can trigger lightning, plus provide a current path to ground.

Like most jet airliners, the shuttle is constructed of conductive aluminum which would normally protect the internal systems. Airplanes are often struck by lightning with no adverse effects because the electricity of the strike is dissipated through the conductive structure and the aircraft is not electrically grounded. The shuttle is not launched under conditions where it could be struck by lightning. Since then, NASA has installed commercial plastic owl decoys and inflatable owl balloons which must be removed prior to launch.

One shuttle launch was delayed in 1995 when a pair of woodpeckers drilled almost 200 holes into the foam insulation of Discovery's external tank. When CNN reported on the breakup of the Columbia over Texas, they erroneously reported it was traveling at nearly 18 times the speed of light, instead of 18 times the speed of sound. (source : John Young's April 2003 After Dinner Speech). On the same subject, a little-publicised detail about the first Shuttle mission, STS-1, was that it had a protruding gapfiller that ducted hot gas into the right wheel well on re-entry, buckling the right main gear on landing as a result.

This image from the NASA archives shows many missing tiles on the STS-1 OMS pods : [[5]] The problem on Columbia was that the damage was sustained to the carbon-carbon leading edge panel of the wing, not the heat tiles. STS-1, STS-16 and STS-41 have all flown with missing thermal tiles from the orbital maneuvering system pods (visible to all the crew). In fact Shuttles had come back missing as many as 20 tiles without any problem. The subject of missing or damaged thermal tiles on the Shuttle fleet only became an issue following the loss of Columbia in 2003 as it broke up on re-entry.

At the point when it is perfectly vertical, the boosters ignite and the launch commences. This takes approximately 6 seconds. As the boosters flex back into their original shape, the launch stack springs slowly back upright. After main engine start, but while the solid rocket boosters are still clamped to the pad, the offset thrust from the Shuttle's three main engines causes the entire launch stack (boosters, tank and shuttle) to flex forwards about 2 meters at the cockpit level.

When watching a launch, look for the "nod" ("Twang" in "NASAese"). NASA was one of its main customers. The Compass sold poorly, because it cost at least $8000, but offered unmatched performance for its weight and size. Early Shuttle missions took along the GRiD Compass, arguably the first laptop computer.

This is still lower than the actual approximately $100 million per launch, but less difference than is commonly thought. Correcting for inflation to 2005 dollars, this equates roughly to $36 million incremental costs per launch. Early cost estimates of $118 per pound of payload were based on marginal or incremental launch costs, and based on 1972 dollars and assuming a 65,000 pound payload capacity. Some early hypothetical studies examined 55 launches per year, but the maximum possible launch rate was limited to 24 per year, based on manufacturing capacity of the external tank.

This does not reduce actual operating costs, but if dividing total program costs by number of launches, more launches per year produces a lower per-launch cost figure. Launch rate is significantly lower than initially expected. Before the current "Block II" engines, the turbopumps (a primary engine component) had to be removed, dissembled, and totally overhauled after each flight. The main engines were highly complex and maintenance intensive, necessitating removal and extensive inspection after each flight.

Maintenance of thermal protection tiles turned out to be very labor intensive, averaging about 1 person·week to replace a tile, with hundreds damaged with each launch. Columbia — lost during reentry, February 1, 2003. Challenger — lost 73 seconds after liftoff, January 28, 1986. Ulysses probe.

Galileo spacecraft. Magellan probe. An interplanetary orbit; these have included: