SpaceX

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This article contains information regarding an LSP that is scheduled to conduct a launch in the next 15 days.

Details may change as the countdown and ascent progress. Launch details: SpaceX will use a Falcon 1 to launch Trailblazer and two CubeSats for the American Air Force and MDA, and for Malaysia's ATSB. Launch will occur from Omelek Island at Kwajalein Atoll. A Celestis Space burial payload, Explorers, including the remains of astronaut Gordon Cooper and Star Trek actor James Doohan is also being flown. If the launch is successful, it will be the first privately funded liquid-fuelled rocket to reach low Earth orbit.

Launch is scheduled for 23 June 2008 at 23:00 UTC. See 2008 in spaceflight and the Spaceflight Portal for further details.

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SpaceX
Type	Private
Founded	2002
Headquarters	Hawthorne, California
Key people	Elon Musk: CEO and CTO
Industry	Aerospace
Products	Orbital rocket launch
Revenue	unknown
Employees	400
Website	spacex.com

The Space Exploration Technologies Corporation (SpaceX) is a space-transportation startup company founded by Elon Musk. Its goal is to improve the cost and reliability of access to space by a factor of ten. It is developing partially reusable two-stage kerosene–liquid-oxygen launch vehicles. It was based in El Segundo, but moved to a former Boeing factory in Hawthorne, California, USA.

1 Background
2 Launcher versions
3 Launches
4 Future development
- 4.1 Heavy lift launchers
- 4.2 Manned orbital spaceflight: SpaceX Dragon
5 Space Industry Partnerships
6 External links
- 6.1 Articles
7 Notes

[edit] Background

SpaceX was founded in June 2002 by Musk, who is CEO and CTO. Musk co-founded startup companies Zip2 and PayPal and is chairman of Tesla Motors and SolarCity. As of March 2006 he had invested $100,000,000 of his money.

There were 160 employees in November 2005^[1], and 400 by November 2007.^[2] The launch crew in the Marshall Islands has 25 people, 6 in mission control. This small number, compared to companies with similar rockets, is part of cost reduction. Musk sees other space-launch services' high prices as supporting unnecessary bureaucracy.

[edit] Launcher versions

Version	Falcon 1	Falcon 9	Falcon 9 Heavy
Stage 0	none	none	2 boosters with 9 × Merlin 1C each
Stage 1	1 × Merlin	9 × Merlin 1C	9 × Merlin 1C
Stage 2	1 × Kestrel	1 × Merlin 1C	1 × Merlin 1C
Height (max; m)	between 21.3 and 26.83	50 or 54	54
Diameter (m)	1.7	3.6	3.6
Initial thrust (kN)	between 318 and 454	3,400	12,258
Takeoff weight (tonnes)	between 27.2 and 38.56	325	885
Fairing diameter (Inner; m)	1.5 or 1.71	3.6 or 5.2	5.2
Payload (LEO; kg)	between 570 and 700 (or 430 to SSO)	9,900	27,500
Payload (GTO; kg)	—	4,900	12,000
Price (Mil. USD)	between 6.7 and 8.5	35 to LEO or GEO	90 to LEO or between 55 and 90 (according to Satellite Mass) to GEO
minimal Price/kg (LEO; USD)	between 11,754 and 15,556 (or 19,767 to SSO)	3,365	3,273
minimal Price/kg (GTO; USD)	—	10,000	7,826
Success ratio (successful/total)	0/2	—	—

^[3] ^[4] ^[5] ^[6] ^[7]

A Falcon 5 launcher was planned, but development was stopped.

[edit] Launches

[edit] Maiden test flight of Falcon 1

Falcon 1 prototype.

The first Falcon 1 at Space Launch Complex—Three West (SLC-3W), Vandenberg Air Force Base.

On November 26, 2005, the first launch attempt was scrubbed due to weather and ground holds. On December 19, 2005, a second scrub occurred when a faulty valve caused the first-stage kerosene tank to deform during an unfueling maneuver. The launch tower was redesigned to reduce liquid-oxygen boil-off and to avoid wind-related holds. On February 10, 2006, further static testing led to a delay. On March 17 and March 22 two static firings validated the rocket hardware and the launch procedures.

The Falcon 1 maiden flight was scheduled for 21:00 UTC on 24 March 2006 (08:00 local time, 25 March). A ship to recover the first stage -- in a restricted down range zone -- caused a 90 minute lauch hold. Launch was at 22:30 UTC (09:30 local time, 25 March), from Omelek Island, in the Kwajalein Atoll.

After 29 seconds (T plus 00:00:29) the main engine failed, leading to vehicle loss soon after. Photography shows the engine on fire during ascent. An investigation by SpaceX and DARPA determined that corrosion on an aluminum nut led to a failure, resulting in a fuel leak. Corrective actions included replacing similar nuts with welding where possible, or with stainless steel nuts, otherwise.^[8] There was a webcast of the flight from launchpad cameras, with mission-control voiceover, showing water-dump, ignition, and pad liftoff. The view switched to an onboard camera, with the atoll receding in the background. The webcast stopped 40 seconds into the flight.

The 19.5-kilogram (43-pound) United States DARPA payload FalconSAT-2 was built by United States Air Force Academy cadets to investigate "space weather", or plasma in the upper atmosphere. The planned orbit was 450 kilometers (280 miles).

[edit] Second test flight of Falcon 1

The second Falcon 1 launched a demonstration payload to return data on the booster's performance, however it failed to reach orbit. The second stage was shut down a minute and a half before schedule (T+ 7:30) due to a control issue. ^[9] SpaceX later stated that "The second stage was otherwise functioning well and even deployed the satellite mass simulator ring at the end of flight! Actual final velocity was 5.1 km/s or 11,000 mph, whereas 7.5 km/s or 17,000 mph is needed for orbit."

The first launch attempt was targeted for 2300 UTC, 20 March 2007 however it was aborted one minute and two seconds prior to launch (T minus 00:01:02) due to a ground control software handover failure. A second attempt was made at 00:05 UTC, 21 March 2007, but the launch was aborted automatically 0.5 seconds after firing the engines because the main engine chamber pressure was about 0.2 percent lower than allowable. The low pressure was caused by the fuel being colder than desired. The third attempt successfully launched the rocket at 01:10 UTC, 21 March 2007 (13:10 local time, 20 March 2007), the vehicle separated from the first stage booster and fairing at approximately 6:14 PST.

The webcast from the vehicle was lost at T+ 5:05 at an altitude of approximately 300 kilometers, but SpaceX was able to retrieve telemetry for the entire mission. The video showed a coning motion that increased during the second stage burn, then a roll immediately before loss of signal.^[10] Musk noted that the control problem was initiated during stage separation, when the shut down kick of the main engine exceeded their predictions. This caused a bump between the first stage and second stage engine nozzle, along with sloshing in the tanks. The vehicle's systems were designed to damp out sloshing, but the unexpected motion exceeded design parameters. ^[9]

SpaceX stated they were happy with the launch as the rocket reached space and validated the riskiest and most difficult parts of the new design. Musk expressed confidence that they would solve the control issue and noted that all new rockets typically have these problems to work out; "I think they had something like 12 Atlas failures before the 13th one was success. To get this far on our second launch being an all-new rocket -- new main engine, new first stage, new second stage engine, new second stage, new fairing, new launch pad system, with so many new things -- to have gotten this far is great." ^[11] A post-mission report declared this launch "the end of the test phase for Falcon 1 and the beginning of the operational phase." ^[12]

[edit] Upcoming launches

The third Falcon 1 launch is planned for 23 June 2008, at 23:00 GMT, from Kwajalein.^[13] This flight will carry the Trailblazer (Jumpstart-1) satellite for the US Air Force, two cubesats for ATSB of Malaysia, and a Space Burial payload for Celestis.

The maiden launch of the Falcon 9 is scheduled for the fourth quarter of 2008 with a U.S. government payload, followed closely by the launch of a payload for the Canadian MDA Corporation.^[14]^{[dubious – discuss]}

On May 2, 2005, SpaceX announced that it had been awarded an Indefinite Delivery/Indefinite Quantity (IDIQ) contract for Responsive Small Spacelift (RSS) launch services by the United States Air Force, which could allow the Air Force to purchase up to $100,000,000 worth of launches from the company.^[15] On April 22, 2008, NASA announced that it had awarded an IDIQ Launch Services contract to SpaceX for Falcon 1 and Falcon 9 launches. The contract will be worth between $20,000 and $1 billion, depending on the number of missions awarded. The contract may cover launch services through June 30, 2010, for launches through December 2012.^[16]

Ellon Musk stated in the same April 22 announcement on the company's webpage that SpaceX has sold 14 contracts for flights on the various Falcon vehicles.^[17]

[edit] Future development

[edit] Heavy lift launchers

On September 8, 2005, SpaceX announced the development of the Falcon 9 rocket, which will have nine Merlin engines in its first stage.^[18]^[19] The design is an EELV-class vehicle, intended to compete with the Delta IV and the Atlas V rockets. Both stages will be designed to be reusable. A similarly designed Falcon 5 rocket was also envisioned to fit between the Falcon 1 and Falcon 9, but development was dropped to concentrate on the Falcon 9.

The company purchased the McGregor, Texas testing facilities of defunct Beal Aerospace, where it is refitting the largest test stand at the facilities for Falcon 9 testing. The stand will test the 9 Merlin 1C engines of the Falcon 9, which will deliver 350-metric-tons-force (3.4-meganewtons) of thrust, well under the stand's capacity of 1,500 metric-tons-force (15 meganewtons).

SpaceX plans to develop the Merlin 2 engine^{[citation needed]}, a scale version of a larger F-1-class engine. The company is rumored to be working on a very large rocket to accompany the F-1-class engine, known by the codename "BFR" (Big Falcon Rocket). ^[20] Musk said "Long-term plans call for development of a heavy lift product and even a super-heavy, if there is customer demand. We expect that each size increase would result in a meaningful decrease in cost per pound to orbit. For example, dollar cost per pound to orbit dropped from $4,000 to $1,300 ($8,800/kg to $2,900/kg) between Falcon 1 and Falcon 5. Ultimately, I believe $500 per pound ($1,100/kg) or less is very achievable." Musk said he expects to offer $1,000 per kilogram by 2010.^{[citation needed]}

[edit] Manned orbital spaceflight: SpaceX Dragon

Main article: SpaceX Dragon

SpaceX announced plans to pursue a manned commercial space program through the end of the decade.^[21]

On Friday 18 August 2006, NASA announced that the company was one of two selected to provide crew and cargo resupply demonstration contracts to the International Space Station (ISS) under the Commercial Orbital Transportation Services (COTS) program. SpaceX will demonstrate crew and cargo resupply using the SpaceX Dragon, a conventional blunt-cone ballistic capsule, which is capable of carrying 7 persons or a mixture of personnel and cargo to and from low Earth orbit.^[22] It will be launched atop a Falcon 9 vehicle. The nosecone of the vehicle has a hinged cap, which opens to reveal a standard ISS Common Berthing Mechanism, which allows the Dragon to dock to the U.S. segment of the ISS. NASA's plan calls for SpaceX demonstration flights between 2008 and 2010. SpaceX may receive up to $278 million if it meets all NASA milestones.^[23]^[24]^[25]