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Falcon 9 Block 5

From Wikipedia, the free encyclopedia
Fifth version of the SpaceX medium-lift launch vehicle

Falcon 9 Block 5
On one side is an Falcon 9 carrying theCrew-10 mission to ISS while on the other side is an Falcon 9 carrying theIMAP,SWFO-L1 andCarruthers Geocorona Observatory and spacecraft to Sun-Earth Lagrange point.
FunctionMedium-lift launch vehicle
ManufacturerSpaceX
Country of originUnited States
Cost per launchUS$69.75 million (2024)[1]
Size
Height
  • 69.8 m (229 ft) with payload fairing
  • 65.7 m (216 ft) withDragon 2[a][2]
Diameter3.7 m (12 ft)[3]
Mass549,000 kg (1,210,000 lb)[3]
Stages2
Capacity
Payload toLEO
Orbital inclination28.5°
Mass
  • Expended: 22,800 kg (50,300 lb)[1]
  • Reusable: 18,500 kg (40,800 lb)[4]
Payload toGTO
Orbital inclination27°
Mass
  • Expended: 8,300 kg (18,300 lb)[1]
  • Reusable: 5,500 kg (12,100 lb)[1]
Payload toTMI
Mass4,000 kg (8,800 lb)[1]
Associated rockets
FamilyFalcon 9
Based onFalcon 9 Full Thrust
Comparable
Launch history
StatusActive
Launch sites
Total launches512
Success(es)511
Failure1 (Starlink Group 9‑3[b])
Landings513 / 519 attempts[c]
First flightMay 11, 2018 (Bangabandhu-1)
Last flightNovember 23, 2025(most recent)
Carries passengers or cargo
First stage
Height41.2 m (135 ft)
Powered by9 ×Merlin 1D
Maximum thrust7,600 kN (1,700,000 lbf)[5][6]
PropellantLOX /RP-1[7]
Second stage (standard)
Height13.8 m (45 ft 3 in)
Powered by1 ×Merlin 1D Vacuum
Maximum thrust934 kN (210,000 lbf)[3]
PropellantLOX /RP-1
Second stage (short nozzle)
Height13.6 m (44 ft 7 in)
Powered by1 ×Merlin 1D Vacuum
Maximum thrust840 kN (190,000 lbf)[3]
PropellantLOX /RP-1

Falcon 9 Block 5 is apartially reusable,human-rated,two-stage-to-orbit,medium-lift launch vehicle[d] designed and manufactured in the United States bySpaceX. It is the fifth major version of theFalcon 9 family and the third version of theFalcon 9 Full Thrust.[8][9] It is powered byMerlin 1D engines burning rocket-grade kerosene (RP-1) andliquid oxygen (LOX).

The main changes from Block 3 (the original Falcon 9 Full Thrust) to Block 5 are higher-thrust engines and improvements to the landing legs along with numerous other small changes to streamline recovery and re-use offirst-stage boosters and increase the production rate. Each Block 5 booster is designed to fly ten times with only minor maintenance between launches and potentially up to 100 times with periodic refurbishment.

In 2018, Block 5 succeeded the transitional Block 4 version. The maiden flight of the Block 5 launched the satelliteBangabandhu-1 on May 11, 2018. TheCRS-15 mission on June 29, 2018, was the last to be launched on a Block 4 rocket, completing the transition to an all-Block 5 fleet.[10][11]

Overview

[edit]

The Block 5 design changes are principally driven by upgrades needed for NASA'sCommercial Crew program andNational Security Space Launch requirements.[12] They include performance upgrades, manufacturing improvements, and increase the margin for demanding customers.[13]

In April 2017, SpaceX CEOElon Musk said that Block 5 will feature 7–8% more thrust by uprating the engines (from 176,000 pounds-force (780,000 N) to 190,000 pounds-force (850,000 N) per engine).[14] Block 5 includes an improved flight control system for an optimizedangle of attack on the descent, lowering landing fuel requirements.

For reusability endurance:

  • expected to be able to fly ten times with only minor maintenance between launches[15][16] achieved in 2021[17]
  • potentially fly up to 100 times with periodic refurbishment[16][15][18]
  • a reusable heat shield protecting the engines and plumbing at the base of the rocket;
  • more temperature-resistant cast and machinedtitanium grid fins;[19]
  • a thermal-protection coating on the first stage to limit reentry heating damage, including a black thermal protection layer on the landing legs, raceway, and interstage;
  • redesigned and requalified more robust and longer life valves;
  • redesignedcomposite overwrapped pressure vessels (COPV 2.0) forhelium, to avoid oxygen freezing inside the structure of the tanks that lead to rupture.

For rapid reusability:

  • reduced refurbishment between flights;[16]
  • a set of retractable landing legs for rapid recovery and shipping.[20]
  • the Octaweb[21] structure is bolted together instead of welded, reducing manufacturing time.[22]

Improvements

[edit]

Since the debut of Block 5, SpaceX has continued to iterate on its design, manufacturing processes, and operational procedures.[23] Among other changes, the initial Block 5 boosters did not have the redesignedcomposite overwrapped pressure vessel (COPV2) tanks.[24] The first booster with COPV2 tanks was booster B1047 on theEs'hail 2 mission on November 15, 2018, and the second booster using the COPV2 tanks wasCRS-16/B1050, which had its first launch on December 5, 2018.[25] Later Block 5 boosters are also easier to prepare for flight, so SpaceX "prefer to retire" older cores by assigning them to expendable missions when possible.[26]

A pressure relief valve was added to the grid fins’ hydraulic system following a stall that resulted in a landing failure in 2018.[27][28] Similarly, after a booster was damaged at sea in 2022, much of the fleet was upgraded with "self-leveling" landing legs. These legs help ensure the booster can be properly secured to the Octograbber, even in suboptimal sea states.[29]

To improve the rocket's performance, SpaceX has tweaked throttle settings and separation timings.[23][30]

Mission extension kits

[edit]

SpaceX CRS-18 featured a Falcon mission-extension kit to the standard second stage, which equipped the second stage with a dark-painted band (for thermal control), extraCOPVs for pressurization control, and additionalTEA-TEB ignition fluid. The upgrades afforded the second stage with the endurance needed to inject the payloads directly into geosynchronous or high energy orbit where the second stage needs hours after launch.[31] Based on mission requirements, they are Medium Coast & Long Coast kits, i.e., the number of helium bottles for pressurization and added batteries for power and other hardware to make sure that the fuel and stages systems operate as long as needed.[32][33]

Short nozzle second stage

[edit]

TheTransporter-7 mission marked the debut of a second stage with aMerlin 1D Vacuum engine with a shorter nozzle extension designed to accelerate production and reduce costs. Unlike the first stage, the second stage on the Falcon 9 is not reused. This variant sacrifices 10% thrust in exchange for a 75% reduction in material usage, primarily the rare metalniobium. As a result, SpaceX can triple its launch frequency using the same amount of this critical resource. Due to its reduced performance, this nozzle is exclusively used on missions with lower performance requirements.[32][34]

Human rating

[edit]

The NASA certification processes of the 2010s specified seven flights of any launch vehicle without major design changes before the vehicle would beNASA-certified for human spaceflight, and allowed to fly NASA astronauts.[24][25]

The Block 5 design launched astronauts for the first time on May 30, 2020, on a NASA-contracted flight,Crew Dragon Demo-2.[35] This was the first crewed orbital spaceflight launched from the United States since thefinal Space Shuttle mission in 2011, and the first ever operated by a commercial provider.[36]

Specifications

[edit]

Specifications and characteristics are as follows:[37][38][39]

CharacteristicFirst stageSecond stage
Height[39]42.6 m (140 ft)12.6 m (41 ft)
Diameter[39]3.7 m (12 ft)3.7 m (12 ft)
Empty mass[e][39]22,200 kg (48,900 lb)4,000 kg (8,800 lb)
Gross mass[f]433,100 kg (954,800 lb)111,500 kg (245,800 lb)
Structure typeLOX tank:monocoque
Fuel tank: skin andstringer
LOX tank: monocoque
Fuel tank: skin and stringer
Structure materialAluminum lithium skin;aluminum domes
Engines9 ×Merlin 1D1 ×Merlin 1D Vacuum
Engine typeLiquid,gas-generator
FuelKerosene (RP-1)
OxidizerSubcooledliquid oxygen (LOX)Liquid oxygen (LOX)
LOX tank capacity[39]287,400 kg (633,600 lb)75,200 kg (165,800 lb)
RP-1 tank capacity[39]123,500 kg (272,300 lb)32,300 kg (71,200 lb)
Engine nozzleGimbaled, 16:1 expansionGimbaled, 165:1 expansion
Totalthrust[3]7,607 kN (1,710,000 lbf)934 kN (210,000 lbf)
Propellant feed systemTurbopump
Throttle capability[37]845–482 kN (190,000–108,300 lbf)[40]930–360 kN (210,000–81,000 lbf)
Restart capabilityYes (only 3 engines for boostback/reentry/landing burns)Yes, dual redundantTEA-TEB
pyrophoricigniters
Tank pressurizationHeatedhelium
Ascentattitude control
(pitch,yaw)
Gimbaled enginesGimbaled engine andnitrogengas thrusters
Ascent attitude control
(roll)
Gimbaled enginesNitrogen gas thrusters
Coast/descent attitude controlNitrogen gas thrusters andgrid finsNitrogen gas thrusters
Shutdown processCommanded

Gallery

[edit]

See also

[edit]

Notes

[edit]
  1. ^63.7 m (209 ft) withDragon 1
  2. ^Second stage engine disintegration
  3. ^including use as side booster
  4. ^If launched in expendable configuration, Falcon 9 has a theoretical payload capability of aheavy-lift launch vehicle
  5. ^without propellant
  6. ^with propellant

References

[edit]
  1. ^abcde"Capabilities & Services (2016)". SpaceX. November 28, 2012. Archived fromthe original on August 2, 2013. RetrievedMay 3, 2016.
  2. ^"Falcon User's Guide"(PDF). January 14, 2019. Archived fromthe original(PDF) on December 2, 2020. RetrievedFebruary 26, 2019.
  3. ^abcde"Falcon 9". SpaceX. November 16, 2012. RetrievedApril 30, 2016.
  4. ^Sesnic, Trevor (February 25, 2024)."Starlink Group 6-39 – Falcon 9 Block 5".Everyday Astronaut. RetrievedFebruary 25, 2024.
  5. ^SpaceX (May 11, 2018)."Bangabandhu Satellite-1 Mission". RetrievedFebruary 25, 2019 – via YouTube.
  6. ^SpaceX."FALCON 9". SpaceX. Archived fromthe original on July 15, 2013. RetrievedMarch 2, 2019.
  7. ^@elonmusk (December 17, 2015)."-340 F in this case. Deep cryo increases density and amplifies rocket performance. First time anyone has gone this low for O2. [RP-1 chilled] from 70F to 20 F" (Tweet). RetrievedDecember 19, 2015 – viaTwitter.
  8. ^"Falcon 9 & Falcon Heavy". Archived fromthe original on July 21, 2020. RetrievedFebruary 3, 2021.The v1.2 design was constantly improved upon over time, leading to different sub-versions or "Blocks". The initial design, flying on the maiden flight, was thus referred to as Block 1. The final design which has largely stayed static since 2018 is the Block 5 variant.
  9. ^"Acme Engineering". RetrievedFebruary 3, 2021.
  10. ^Ralph, Eric (June 5, 2018)."SpaceX will transition all launches to Falcon 9 Block 5 rockets after next mission".TESLARATI.com. RetrievedFebruary 26, 2019.
  11. ^Shanklin, Emily (June 29, 2018)."Dragon Resupply Mission (CRS-15)".SpaceX. Archived fromthe original on May 24, 2019. RetrievedFebruary 26, 2019.
  12. ^"Falcon-9 v1.2 (Block 5) (Falcon-9FT (Block 5))".Gunter's Space Page. RetrievedJune 27, 2022.
  13. ^NASA (February 17, 2017)."NASA Holds Pre-launch Briefing at Historic Pad 39A at Kennedy Space Center".Youtube.Public Domain This article incorporates text from this source, which is in thepublic domain.
  14. ^Clark, Stephen (April 4, 2017)."Musk previews busy year ahead for SpaceX".Spaceflight Now. RetrievedApril 7, 2018.
  15. ^abSpaceX Test-Fires New Falcon 9 Block 5 Rocket Ahead of Maiden Flight (Updated). Robin Seemangal,Popular Mechanics. May 4, 2018.
  16. ^abcSpaceX is about to land a whole lot more rockets. Loren Grush,The Verge. July 22, 2018.
  17. ^"SpaceX flies historic 10th mission of a Falcon 9 as Starlink constellation expands". May 8, 2021. RetrievedJuly 1, 2021.
  18. ^Elon Musk on Twitter:I don't want be cavalier, but there isn't an obvious limit. 100+ flights are possible. Some parts will need to be replaced or upgraded.
  19. ^Musk, Elon (June 24, 2017)."Flying with larger & significantly upgraded hypersonic grid fins. Single piece cast & cut titanium. Can take reentry heat with no shielding".@elonmusk. RetrievedMarch 16, 2018.
  20. ^"SpaceX Test-Fires New Falcon 9 Block 5 Rocket Ahead of Maiden Flight (Updated)". Popular Mechanics. May 4, 2018.
  21. ^"Octaweb Structure".www.thespacetechie.com. July 10, 2021.
  22. ^"I am Andy Lambert, SpaceX's VP of Production. Ask me anything about production & manufacturing, and what it's like to be a part of our team!". reddit.com. April 24, 2018.
  23. ^ab"SpaceX Building Airline-Type Flight Ops For Launch | Aviation Week Network".aviationweek.com. RetrievedJanuary 15, 2023.
  24. ^abClark, Stephen."New helium tank for SpaceX crew launches still waiting to fly – Spaceflight Now". RetrievedDecember 6, 2018.
  25. ^ab"SpaceX landing mishap won't affect upcoming launches".SpaceNews.com. December 5, 2018. RetrievedDecember 6, 2018.
  26. ^Starbase Tour with Elon Musk [PART 2 // Summer 2021], August 7, 2021, retrievedJanuary 15, 2023
  27. ^Elon Musk & NASA/SpaceX DM1 – Post Launch Press Conference. Event occurs at 12:02. RetrievedApril 13, 2024 – via www.youtube.com.
  28. ^Graham, William (December 5, 2018)."Falcon 9 successfully lofts CRS-16 Dragon enroute to ISS – Booster spins out but soft lands in water".NASASpaceFlight.com. RetrievedApril 13, 2024.
  29. ^Dontchev, Kiko [@TurkeyBeaver] (December 26, 2023)."...Tippy boosters occur when you get a certain set of landing conditions that lead to the legs having uneven loading... In this state, securing with the OG is super challenging and often only partial successful. We came up with self leveling legs that immediately equalize leg loads on landing after experiencing a severe tippy booster two years ago on Christmas (first flight of 1069). The fleet is mostly outfitted, but 1058, given its age, was not..." (Tweet) – viaTwitter.
  30. ^Clark, Stephen."SpaceX launches heaviest payload on Falcon 9 rocket – Spaceflight Now". RetrievedJanuary 27, 2023.
  31. ^Ralph, Eric (October 11, 2022)."SpaceX's first Falcon Heavy launch in three years eyes late-October liftoff".TESLARATI. RetrievedOctober 11, 2022.
  32. ^abSesnic, Trevor (July 22, 2023)."EchoStar 24 | Falcon Heavy".Everyday Astronaut. RetrievedJuly 29, 2023.
  33. ^"Falcon rockets use three configurations of their upper stage. How are they different?". July 31, 2023.
  34. ^"Transporter 7". RetrievedMarch 17, 2023.
  35. ^"NASA, Partners Update Commercial Crew Launch Dates – Commercial Crew Program".blogs.nasa.gov. February 6, 2019. RetrievedFebruary 26, 2019.Public Domain This article incorporates text from this source, which is in thepublic domain.
  36. ^"SpaceX Speeding Astronauts to Space Station in Landmark Trip". Bloomberg News. May 30, 2020.
  37. ^ab"Falcon 9 Launch Vehicle Payload User's Guide, Rev 2"(PDF).SpaceX. October 21, 2015. Archived fromthe original(PDF) on March 14, 2017. RetrievedJanuary 27, 2016.
  38. ^"SpaceX Falcon 9 v1.2 Data Sheet".Space Launch Report. August 14, 2017. Archived from the original on November 14, 2015. RetrievedApril 2, 2018.
  39. ^abcdef"Fiche Technique: Falcon-9" [Technical data sheet: Falcon 9].Espace & Exploration (in French). No. 39. May 2017. pp. 36–37. Archived fromthe original on August 21, 2017. RetrievedJune 27, 2017.
  40. ^"Falcon Users Guide"(PDF). Archived fromthe original(PDF) on February 20, 2019. RetrievedFebruary 22, 2019.

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