|Configuration||Falcon Heavy R|
|Date||20:45:00, 6 February 2018|
|Window||2 hours 30 minutes|
|Site||Cape Canaveral, Florida, U.S.|
|Pad||Launch Complex 39|
|Elon Musk's Tesla Roadster|
|Regime||pseudo-Mars transfer orbit|
The Falcon Heavy test flight (also known as Falcon Heavy demonstration mission) was the first attempt by SpaceX to launch a Falcon Heavy rocket on 6 February 2018 at 20:45 UTC. The successful launch introduced the Falcon Heavy as the most powerful rocket in operation, producing five million pounds-force (22 MN) of thrust and having more than twice the lift capacity of the NASA Space Shuttle launch system.
|Wikinews has related news: SpaceX Falcon Heavy rocket shoots Elon Musk’S personal Car or Tesla as it is called into solar orbiting|
The dummy payload for this test flight was Elon Musk's Tesla Roadster, a sports car owned by SpaceX CEO Elon Musk. SpaceX stated that the payload had to be "something fun and without irreplaceable sentimental value". Sitting in the driver's seat of the Roadster is "Starman", a dummy astronaut clad in a SpaceX spacesuit. It has his right hand on the steering wheel and left elbow resting on the open window sill. Starman is named for the David Bowie song "Starman". The car's sound system was looping the symbolic Bowie songs "Space Oddity" and "Life on Mars?".
It was launched with sufficient velocity to escape the Earth and enter an elliptic orbit around the Sun that crosses the orbit of Mars, reaching an aphelion (maximum distance from the Sun) of 1.67 AU. During the early portion of its voyage it functioned as a broadcast device, sending video back to Earth for four hours. The Roadster remains attached to the second stage.
This launcher demonstration made the Roadster the first consumer car sent into space. Three manned rovers were sent to space on the Apollo 15, 16, and 17 missions in the 1970s, and these vehicles were left on the Moon. The Roadster is one of two formerly manned vehicles (albeit not a manned space vehicle) derelict in solar orbit, joining LM-4 Snoopy, Apollo 10's lunar module ascent stage.
Falcon Heavy flew in its reusable configuration, allowing for a landing approach of both side boosters and the central core. The side boosters consisted of two previously flown Falcon 9 first stages, being reused from the CRS-9 mission in July 2016 and the Thaicom 8 launch in May 2016. The central core was newly built because it needs to support stronger forces during ascent, so that a regular first stage could not be used. The upper stage was the same as on a Falcon 9. Side boosters equipped with a nose cone have different aerodynamic properties than the usual Falcon 9 boosters with a cylindric interstage. For this reason, SpaceX equipped them with larger and sturdier grid fins made of titanium, to help guide the atmospheric descent accurately.The central core, however, still used conventional aluminium grid fins, as its aerodynamic properties are very similar to those of a conventional Falcon 9 first stage. The Roadster was mounted on the second stage using a custom-made payload adapter, and encapsulated in a conventional fairing.. Falcon Heavy also supports the launch of Dragon capsules without a fairing.
The Falcon Heavy maiden flight was intended to accomplish several objectives:
The purpose of including the Roadster on the maiden flight was to demonstrate that the Falcon Heavy can launch payloads as far as the orbit of Mars, and it exceeded its projected route by extending its aphelion to near the asteroid belt beyond Mars (with a perihelion at the level of Earth's orbit), but did not test or demonstrate the separation of the second stage and a payload.
The launch occurred at 3:45 PM EST, or 20:45 UTC, from Launchpad 39A at Kennedy Space Center at Cape Canaveral, Florida; the Roadster was successfully placed in its orbit, and its two booster cores returned to land at Landing Zones 1 and 2 several minutes later. The sole objective not completed was the landing of the central core; while its fate was initially ambiguous due to signal loss and heavy smoke, Musk confirmed several hours after the launch that the booster had not survived the recovery attempt. Because two of the three engines necessary to land were unable to reignite, the booster hit the water at 500 kilometres per hour, 100 metres away from the drone ship. The final upper stage transfer burn to solar orbit produced an orbit that will be beyond the orbit of Mars at its furthest point from the sun.
|T−01:28:00||Go/no go for propellant load|
|T−01:25:00||Kerosene loading underway|
|T−00:45:00||Liquid-oxygen loading underway|
|T−00:07:00||Start of engine chill|
|T−00:01:00||Start of pre-launch checks|
|T−00:01:00||Propellant-tank flight pressurisation|
|T−00:00:45||Go/no go for launch|
|T−00:00:05||Start of side-booster engine ignition sequence|
|T−00:00:03||Start of central-core boosters engines ignition sequence|
|T+00:01:06||Max Q (maximal aerodynamic pressure)|
|T+00:02:29||Boosters engines cutoff (BECO)|
|T+00:02:33||Side boosters separate from central core|
|T+00:02:50||Side boosters begin boostback burn|
|T+00:03:04||Central-core engine shutdown/main engine cutoff (MECO)|
|T+00:03:07||Central core and 2nd stage separate|
|T+00:03:15||2nd-stage engine starts|
|T+00:03:24||Central core begins boostback burn|
|T+00:06:41||Side cores begin entry burn|
|T+00:06:47||Central core begins entry burn|
|T+00:08:31||2nd-stage engine cutoff (SECO-1)|
|T+00:28:22||2nd-stage engine restarts|
|T+00:28:52||2nd-stage engine cutoff (SECO-2)|
|Test continued on an experimental 6-hour-long coast in Earth orbit through the Van Allen radiation belts, followed by two burns by the third stage to target a precessing elliptical orbit around the Sun.|
Valuable telemetry data on the performance of the launch system and its components were obtained for all stages of the test flight.
The dummy payload was placed in a heliocentric orbit, with an aphelion of 1.70 AU, beyond Mars. The payload has an orbital period of 1.53 years. The first four hours of the flight were streamed on YouTube.
Both boosters successfully landed almost simultaneously on the ground at Landing Zones 1 and 2 at Cape Canaveral Air Force Station. As the boosters are still of the old Falcon 9 Block 3 type, SpaceX has ruled out using any of their major parts for a third mission. Due to the high cost and lengthy manufactoring process of the gridfins, however, those might be reused on future flights.
The central core attempted to return to the autonomous spaceport drone ship "Of Course I Still Love You"(name of spaceport drone ship) but failed to light two of the three engines during the landing burn. The core crashed into the ocean 100 metres (300 ft) away from the drone ship at 500 kilometres per hour (300 mph), causing damage to two of the drone ship's station-keeping thrusters. According to Elon Musk on the post-flight conference, the central core ran out of triethylaluminum-triethylborane (TEA-TEB) igniter fluid. Musk later stated that the fix to this problem was "pretty obvious", which led many to believe SpaceX was simply going to add more ignition fluid on future missions.
Congratulations @ElonMusk and @SpaceX on the successful #FalconHeavy launch. This achievement, along with @NASA’s commercial and international partners, continues to show American ingenuity at its best!
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