Falcon 1
From Wikipedia, the free encyclopedia
 Falcon 1 rocket. |
|
| Function | Orbital launch vehicle |
|---|---|
| Manufacturer | SpaceX |
| Country of origin | United States |
| Size | |
| Height | 21.3 m (70 ft) |
| Diameter | 1.7 m (5.5 ft) |
| Mass | 38,555 kg (85,000 lb) |
| Stages | 2 |
| Capacity | |
| Payload to LEO | 670 kg (1480 lb) |
| Payload to SSO |
430 kg (990 lb) |
| Launch history | |
| Status | Active |
| Launch sites | Omelek Island Vandenberg AFB |
| Total launches | 5 |
| Successes | 2 |
| Failures | 3 |
| Partial failures | 0 |
| Maiden flight | March 24, 2006 22:30 GMT |
| First stage | |
| Engines | 1 Merlin 1C |
| Thrust | 454 kN (102,000 lbf) |
| Specific impulse | 255 s (sea level) (2.6 kN·s/kg) |
| Burn time | 169 seconds |
| Fuel | RP-1/LOX |
| Second stage | |
| Engines | 1 Kestrel |
| Thrust | 31 kN (7,000 lbf) |
| Specific impulse | 327 s (vacuum) (3.2 kN·s/kg)) |
| Burn time | 378 seconds |
| Fuel | RP-1/LOX |
The Falcon 1 is a partially reusable launch system designed and manufactured by SpaceX. The two-stage-to-orbit rocket uses LOX/RP-1 for both stages, the first powered by a single Merlin engine and the second powered by a single Kestrel engine. It was designed by SpaceX from the ground up and is the first successful fully liquid-propelled orbital launch vehicle developed with private funding.
The Falcon 1 achieved orbit on its fourth attempt, on 28 September 2008, with a mass simulator as a payload. On 14 July 2009, Falcon 1 successfully delivered the Malaysian RazakSAT satellite to orbit on SpaceX's first commercial launch (fifth launch overall).
Contents |
[edit] Design
According to SpaceX, the Falcon 1 is designed to minimize price per launch for low-Earth-orbit satellites, increase reliability, and optimize flight environment and time to launch.[1] It is also intended to verify components and structural design concepts that will be reused in the Falcon 9.
[edit] First stage
The first stage is made from friction-stir-welded aluminum alloy. It employs a common bulkhead between the LOX and RP-1 tanks, as well as flight pressure stabilization. It can be transported safely without pressurization (like the heavier Delta II isogrid design) but gains additional strength when pressurized for flight (like the Atlas II, which could not be transported unpressurized). The resulting design has the highest propellant mass fraction[citation needed] of any current first stage. The parachute system, built by Irvin Parachute Corporation, uses a high-speed drogue chute and a main chute.
[edit] Second stage
The second stage tanks are built with a cryogenic-compatible aluminum–lithium alloy. The helium pressurization system pumps propellant to the engine, supplies pressurized gas for the attitude control thrusters, and is used for zero-g propellant accumulation prior to engine restart. The Kestrel engine includes a titanium heat exchanger to pass waste heat to the helium, thereby greatly extending its work capacity.[2] The pressure tanks are made by Arde corporation and are the same as those used in the Delta IV. They consist of an inconel shell wrapped by a composite.
[edit] Reusability
It is planned that the first stage will return by parachute to a water landing and be recovered for reuse but this has not yet been demonstrated.[3][4] The second stage is not designed to be reusable.[3][4]
[edit] Operation
At launch, the first stage engine (Merlin) is ignited and throttled to full power while the launcher is restrained and all systems are verified by the flight computer. If the systems are operating correctly, the rocket is released and clears the tower in about seven seconds. The first-stage burn lasts about 2:49 minutes. Stage separation is accomplished with explosive bolts and a pneumatically actuated pusher system.
The second stage Kestrel engine burns for about six minutes, inserting the payload into a low Earth orbit. It is capable of multiple restarts.
[edit] Private funding
The Falcon 1 rocket was developed with private funding. The only other orbital launch vehicle to be privately funded and developed is the Pegasus, first launched in 1990; however, it requires a large aircraft as its first stage.[5] The Falcon 1 is also the first partially reusable orbital rocket to be developed without public funding.[6] While the development of Falcon 1 was privately funded, the first two Falcon 1 launches were purchased by the U.S. Department of Defense under a program that evaluates new US launch vehicles suitable for use by DARPA.[7]
[edit] Pricing
SpaceX is one of the few launch system operators that publishes its launch prices. In 2005 Falcon 1 was advertised as costing $5.9 million ($6.4 million when adjusted for inflation in 2009).[8][9] In 2006 until 2007 the quoted price of the rocket when operational was $6.7 million.[10] In late 2009 SpaceX announced new prices for the Falcon 1 and 1e at $7 million and $8.5 million respectively, with small discounts available for multi-launch contracts.[1]
February 8, 2010 pricing from SpaceX website: Falcon 1 - $8.9 million, Falcon 1e - $10.5 million.
[edit] Launch sites
All flights have been launched from Kwajalein Atoll using the SpaceX launch facility on Omelek Island and range facilities of the Reagan Test Site. All upcoming Falcon 1 flights shown on the SpaceX manifest are also planned for Kwajalein. Other launch sites which have been discussed for Falcon 1 flights include:
- Vandenberg Air Force Base Space Launch Complex 3W. According to Elon Musk, SpaceX may be evicted from Vandenberg because of safety concerns expressed by United Launch Alliance, which launches the Atlas V rocket from neighboring site SLC-3E.[11]
[edit] Variants
| Falcon 1 Versions[1][13][14] | Merlin A; 2006–2007 | Merlin C; 2007–2009 | Falcon 1e; 2010 |
|---|---|---|---|
| Stage 1 | 1 × Merlin 1A | 1 × Merlin 1C | 1 × Merlin 1C |
| Stage 2 | 1 × Kestrel | 1 × Kestrel | 1 × Kestrel |
| Height (max; m) |
21.3 | 22.25 | 26.83 |
| Diameter (m) |
1.7 | 1.7 | 1.7 |
| Initial thrust (kN) |
318 | 343 | 454 |
| Takeoff weight (tonnes) |
27.2 | 33.23 | 38.56 |
| Fairing diameter (Inner; m) |
1.5 | 1.5 | 1.71 |
| Payload (LEO; kg) |
570 (less to SSO) | 450 (less to SSO) | 1,010 (430 to SSO) |
| Payload (GTO; kg) |
— | — | — |
| Price (Mil. USD) |
6.7 | 7 | 9.1 |
| minimal Price/kg (LEO; USD) |
11,754 | 15,556 | 9,010 (19,767 to SSO) |
| minimal Price/kg (GTO; USD) |
— | — | — |
| Success ratio (successful/total) |
0/2 | 2/3 | — |
[edit] Launch history
As of 2009, the Falcon 1 has made five launches. The first three failed, however the subsequent two flights were successful, the first successful launch making it the first privately funded and developed liquid-propellent rocket to reach orbit. The fifth launch was its first commercial flight, and placed RazakSAT into low Earth orbit.
| Flight No | Date & Time (GMT) | Payload | Customer | Outcome | Remarks |
|---|---|---|---|---|---|
| 1 | 24 March 2006, 22:30 (25 March, 09:30 local)[citation needed] |
FalconSAT-2 | DARPA | Failure | Engine failure at T+25 seconds Loss of vehicle |
| 2 | 21 March 2007, 01:10 (13:10 local) |
DemoSat | DARPA | Failure | Successful first stage burn[citation needed] and transition to second stage, maximum altitude 289 km Harmonic oscillation at T+5 minutes Premature engine shutdown at T+7 min 30 s Failed to reach orbit Failed to recover first stage Claimed to be a "Partial success" as it gathered enough data for operational flights[15] |
| 3 | 3 August 2008, 03:34[16] (15:34 local) |
Trailblazer | ORS | Failure | Residual stage 1 thrust led to collision between stage 1 and stage 2[17] |
| PRESat | NASA | ||||
| NanoSail-D | NASA | ||||
| Explorers | Celestis[18] | ||||
| 4 | 28 September 2008, 23:15[19][20] (11:15 local/16:15 PDT) |
RatSat | SpaceX | Successful[19] | Initially scheduled for 23-25 Sept, carried dummy payload - mass simulator, 165 kg (originally intended to be RazakSAT) |
| 5 | 14 July 2009[21] 03:35 | RazakSAT | ATSB | Successful[22] | |
|
|
|||||
| 2Q 2010 | TBD | SpaceDev | Scheduled | maiden flight of 1e configuration | |
| 2010-2014 | O2G | Orbcomm[23] | Scheduled | 18 satellites, number of launches to be confirmed | |
| This table: | |||||
[edit] See also
[edit] Notes
- ^ a b c "Falcon 1 Overview". SpaceX. http://www.spacex.com/falcon1.php. Retrieved 2007-05-05.
- ^ "Falcon 1 Flight Three Press Kit" (PDF). SpaceX. http://www.spacex.com/SpaceX_F1-003_PressKit.pdf. Retrieved 2008-09-30.
- ^ a b Brown, Mary Beth (2005-09-08). "SPACEX ANNOUNCES THE FALCON 9 FULLY REUSABLE HEAVY LIFT LAUNCH VEHICLE". El Segundo, CA: SpaceX. http://www.spacex.com/press.php?page=18. Retrieved 2009-11-04.
- ^ a b Clarke, Stephen (2008-09-28). "Sweet success at last for Falcon 1 rocket". SPACEFLIGHT NOW. http://spaceflightnow.com/falcon/004/. Retrieved 2009-11-04.
- ^ "Orbital Marks 25th Anniversary Of Company's Founding". Orbital Sciences. 2007-04-02. http://www.orbital.com/NewsInfo/release.asp?prid=603.
- ^ "Private sector enticing public into final frontier". USAtoday.com. 2005-06-17. http://www.usatoday.com/educate/college/careers/Entreps/6-17-05.htm.
- ^ "Falcon 1 Reaches Space But Loses Control and is Destroyed on Re-Entry". Satnews.com. 2007-03-21. http://www.satnews.com/stories2007/4156/.
- ^ "DoD Small-Rocket Contract Produces Fierce Competition". Space News. 2005-05-23. http://www.space.com/spacenews/archive05/Launch_052305.html.
- ^ "$5900000 in 2005 dollars". Wolfram Alpha. 2009-08-12. http://www.wolframalpha.com/input/?i=%245900000+in+2005+dollars.
- ^ "SpaceX's Inaugural Falcon 1 Rocket Lost Just After Launch". Space.com. 2006-03-24. http://www.space.com/missionlaunches/060324_spacex_failure.html.
- ^ "SpaceX To Try Again Feb. 9". Space News. http://www.space.com/spacenews/archive05/Falcon_010906.html.
- ^ Kelly, John (2007-04-25). "SpaceX cleared for Cape launches". Florida Today. http://www.floridatoday.com/floridatoday/blogs/spaceteam/2007/04/spacex-cleared-for-cape-launches.html.
- ^ "SpaceX Falcon 1 Data Sheet" (PDF). SpaceX. 2008-09-28. http://www.spacex.com/Falcon1DataSheet.pdf.
- ^ "Falcon 1 Users Guide" (PDF). SpaceX. 2008-09-28. http://www.spacex.com/Falcon1UsersGuide.pdf.
- ^ "Demoflight 2 Update". SpaceX. 2007-03-20. http://www.spacex.com/updates.php#demoflight_2_launch_update_12.
- ^ Clark, Stephen (2008-08-03). "Falcon 1 suffers another setback". Spaceflight Now. http://www.spaceflightnow.com/falcon/003/. Retrieved 2008-08-05.
- ^ "Flight 3 mission summary". Space Exploration Technologies Corporation. http://www.spacex.com/updates.php#Update080608.
- ^ a b "Launch Manifest". SpaceX. http://www.spacex.com/launch_manifest.php. Retrieved 2008-08-03.
- ^ a b Ray, Justin (2008-09-28). "Mission Status Center" (in English). Spaceflight Now. http://www.spaceflightnow.com/falcon/004/status.html. Retrieved 2008-09-28.
- ^ "Flight 4 Launch Update". SpaceX. 23 September 2008. http://spacex.com/updates.php.
- ^ "SPACEX And ATSB Announce New Launch Date For Razaksat Satellite". http://www.space-travel.com/.+2009-06-02. http://www.space-travel.com/reports/SPACEX_And_ATSB_Announce_New_Launch_Date_For_Razaksat_Satellite_999.html. Retrieved 2009-06-02.
- ^ [1]
- ^ "SpaceX Wins Orbcomm Contract to Launch 18 Satellite Constellation". Satellite Today. 2009-09-03. http://www.satellitetoday.com/st/topnews/SpaceX-Wins-Orbcomm-Contract-to-Launch-18-Satellite-Constellation_31968.html. Retrieved 2009-09-03.
[edit] Further reading
- "Damage puts first SpaceX rocket launch on hold". Spaceflight Now. 19 December 2005. http://www.spaceflightnow.com/falcon/f1/051219damage.html.
- "SpaceX rocket fails first flight". BBC News. 24 March 2006. http://news.bbc.co.uk/2/hi/science/nature/4698736.stm.
[edit] External links
 |
Wikimedia Commons has media related to: Falcon 1 |
|
||||||||||||||||||||||
|
||||||||||||||||||||||||||||||||||||||||
|
||||||||||||||
