The Sun is good. Without our hot, gas ball of a friend, wed all be dead. More accurately, we would have never been born So its a good thing that our Sun has. IFly. com Airport Info, Flight Status Tracking, Airport Parking, Terminal Maps, Groundtransportation, Flights, Hotels, and more Info. Dragon 2 Wikipedia. This article is about the Space. X space capsule. For the Dragon 2 biplane, see de Havilland Dragon. Space. X Dragon 2. Dragon 2 spacecraft in a test chamber on top of the trunk. Manufacturer. Space. XCountry of origin. United States. Operator. Applications. ISS crew transfer. Space tourism to lunar orbit. SgTkQda.jpg' alt='Star Ocean First Departure Walkthrough Pdf' title='Star Ocean First Departure Walkthrough Pdf' />Specifications. Spacecraft type. Crewed capsule. Design life. Dry massabout 6,4. Payload capacity. Star Ocean First Departure Walkthrough Pdf' title='Star Ocean First Departure Walkthrough Pdf' />ISS2,5. Crew capacity. 7Dimensions. Diameter 3. 7 m 1. Height 8. 1 m 2. Sidewall angle 1. Volume. 10 m. 3 3. Regime. Production. Star Ocean First Departure Walkthrough Pdf' title='Star Ocean First Departure Walkthrough Pdf' />Status. In development. Built. Dragon. FlyFirst launch. August 2. 01. 8 planned5Dragon 2 also Crew Dragon, Dragon V2, or formerly Dragon. Rider is the second version of the Space. X Dragon spacecraft, which will be a human rated vehicle. Car Restore Game there. It includes a set of four side mounted thruster pods with two Super. Draco engines each, which can serve as a launch escape system or launch abort system LAS or potentially be used for propulsive landings. Also, it has much larger windows, new flight computers and avionics, and redesigned solar arrays, and a modified outer mold line from the initial cargo Dragon that has been flying for several years. The spacecraft was unveiled on May 2. Space. X headquarters in Hawthorne, California. Designed to ferry astronauts to space, the capsule differs considerably from the cargo carrying Dragon, which has been operational since 2. As of October 2. 01. International Space Station ISS in April 2. August 2. 01. 8. 5Space. X completed a launch pad abort test of the spacecraft on 6 May 2. November 2. 01. 5. NASA has signed a contract to procure up to six crewed flights to the International Space Station under the Commercial Crew Development. Dragon 2 development historyedit. Dragon. Rider mockup, showing the launch escape system engines mounted on the outside of the capsule, when the design was not yet final. Crewed version of Dragon CRS with powered vertical landing ability. The crewed variant of Dragon was initially called Dragon. Rider. 1. 3 It was intended from the beginning to support a crew of seven or a combination of crew and cargo. It was planned to be able to perform fully autonomous rendezvous and docking with manual override ability and was designed to use the NASA Docking System NDS to dock to the ISS. For typical missions, Dragon. Rider would remain docked to the ISS for a period of 1. Russian Soyuz spacecraft. From the earliest design concepts which were publicly released in 2. Space. X planned to use an integrated pusher launch escape system for the Dragon spacecraft, claiming several advantages over the tractor detachable tower approach used on most prior crewed spacecraft. These advantages included the provision for crew escape all the way to orbit, reusability of the escape system, improved crew safety due to eliminating a stage separation, and the ability to use the escape engines during landings for a precise solid earth landing of the capsule. Space. X originally intended to certify their propulsive landing scheme, in parallel with the parachute to water landing method for Dragon 2, with the goal to hold to the development schedule and ensure U. S. crew transportation safely and reliably in 2. Space. X announced that land landing will become the baseline for the early post certification missions while precision water landing under parachutes was proposed to NASA as the baseline return and recovery approach for the first few flights of Crew Dragon. Thus the parachute system was initially anticipated to be only a backup system due to the cancellation of propulsive landing, however, the parachute system will be used for all landings. As of 2. 01. 1update, the Paragon Space Development Corporation was assisting in developing Dragon. Riders life support system. In 2. 01. 2, Space. X was in talks with Orbital Outfitters about developing space suits to wear during launch and re entry. At a NASA news conference on 1. May 2. 01. 2, Space. X confirmed again that their target launch price for crewed Dragon flights is 1. NASA orders at least four Dragon. Rider flights per year. This contrasts with the 2. Soyuz launch price of 7. NASA astronauts. 2. In October 2. 01. NASA selected the Dragon spacecraft as one of the candidates to fly American astronauts to the International Space Station under the Commercial Crew Program. Space. X plans to use the Falcon 9 Block 5 launch vehicle for launching Dragon 2. Technical specificationseditDragon 2 includes the following features 89Reuses partly reusable can be flown multiple times, resulting in a significant cut in the cost of access to space. Space. X anticipates that about ten flights are possible before significant vehicle refurbishing is needed. Capacity seven astronauts. Landing four main parachutes for water landing possibility of developing propulsive landing using the Super. Draco engines. Engines eight side mounted Super. Draco engines, clustered in redundant pairs in four engine pods, with each engine able to produce 7. Each podcalled a quad by Space. Xcontains two Super. Draco engines plus four Draco thrusters. Nominally, only two quads are used for on orbit propellant with the Dracos and two quads are reserved for propulsive landing using the Super. Dracos. 2. 5The first fully printed engine, the Super. Draco Engine combustion chamber is printed of Inconel, an alloy of nickel and iron, using a process of direct metal laser sintering. Engines are contained in a protective nacelle to prevent fault propagation if an engine fails. Docking able to autonomouslydock to space stations. Dragon V1 used berthing, a non autonomous means to attach to the ISS that was completed by use of the Canadarm. Pilot ability to park the spacecraft using manual controls if needed. Reservoirs composite carbon overwrap titanium spherical tanks to hold the helium used to pressurize engines and also for the Super. Draco fuel and oxidizer. Shield updated third generation PICA Xheat shield. Controls tablet like computer that swivels down for optional crew control by the pilot and co pilot. Interior design tan leather seatsthe spacecraft can be operated in full vacuum, and the crew will wear Space. X designed space suits to protect them from a rapid cabin depressurization emergency event. Also, the spacecraft will be able to return safely if a leak occurs of up to an equivalent orifice of 0. Movable ballast sled to allow more precise attitude control of the spacecraft during the atmospheric entry phase of the return to Earth and more accurate control of the landing ellipse location. Reusable nose cone the second structural element of the spacecraft, which protects the vessel and the docking adaptor during ascent and reentry2. Trunk the third structural element of the spacecraft, which contains the solar arrays, heat removal radiators, and will provide aerodynamic stability during emergency aborts. The landing system was initially designed to accommodate three types of landing scenarios Propulsive landing, for vertical takeoff, vertical landing VTVLParachute landing, similar to prior American manned space capsules. Parachute landing with propulsive assist, similar to that used by the Soyuz spacecraft The whole landing system is designed so that its survivable if theres no propulsive assist at all.