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VLS-1

From Wikipedia, the free encyclopedia
Brazilian Space Agency satellite launcher
For the naval missile-firing system, seeVertical launching system.
VLS-1
Veículo Lançador de Satélites
VLS-1
FunctionOrbitallaunch vehicle
ManufacturerCTA
Country of originBrazil
Size
Height19.5 m (64 ft)
Diameter1.01 m (3.3 ft)
Mass50,700 kg (111,800 lb)
Stages3
Capacity
Payload tolow Earth orbit
Mass380 kg (840 lb)
Launch history
StatusCancelled[1]
Launch sitesAlcântara VLS Pad
Total launches2
Success(es)0
Failure2
Notable outcome1 (pad explosion in 2003)
First flight2 November 1997
(VLS-1 V01)
Last flight11 December 1999
(VLS-1 V02)
Boosters – S-43
No. boosters4
Powered by1solid rocket booster
Total thrust303 kN (68,000 lbf)
Specific impulse225 s (2.21 km/s)
Burn time59 seconds
First stage – S-43TM
Powered by1solid rocket booster
Specific impulse277 s (2.72 km/s)
Burn time58 seconds
Second stage –S-40TM
Powered by1solid rocket booster
Specific impulse275 s (2.70 km/s)
Burn time56 seconds
Third stage –S-44
Powered by1solid rocket booster
Specific impulse282 s (2.77 km/s)
Burn time68 seconds

TheVLS-1 (Portuguese:Veículo Lançador de Satélites) was theBrazilian Space Agency's mainsatellite launch vehicle.[2] The launch vehicle would have been capable of launchingsatellites intoorbit. The launch site was located at theAlcântara Launch Center[3] due to its proximity to theequator.

Associated vehicles include theSonda I,Sonda II,Sonda III andSonda IV, theVS-30,VS-40 andVSB-30.

The VLS was cancelled after decades of development and high expenditures with poor results and a failed association with Ukraine that slowed the program for years.[4][1]

History

[edit]

VLS-1 development started in 1984, after the first launch of the Sonda IV rocket. To date, three prototypes have been built and two launches attempted, departing from the Alcântara Launch Center. During the V1 and V2 prototype launches (VLS-1 V1 and VLS-1 V2) technical problems prevented mission success, but allowed the testing of several vehicle components. The V3 prototype exploded on the launch pad on 22 August 2003, two days before its intended launch date. The2003 Alcântara VLS accident caused a considerable setback to the Brazilian space program. The V4 prototype was expected to be launched in 2016.[5]

The project was terminated by Brazilian Space Agency in 2016.[6]

TheDepartamento de Ciência e Tecnologia Aeroespacial (DCTA) (Department of Aerospace Science and Technology) and theAgência Espacial Brasileira (AEB) (Brazilian Space Agency) informed on public audience before the VLS-1 project ended by theSenado Federal (Federal Senate) on February 16, 2016.[citation needed]

VLS-1 schedule

[edit]

Initial flight test schedule

[edit]
#PhotoVehiclePayloadDatePlaceResult
1VLS-R1-1985 December 1CLAFailure, apogee of 10 km.
2VLS-R2-1989 May 18CLAApogee of 50 km.
3VLS-1 V01SCD-2A1997 November 2CLAin-flight failure
4VLS-1 V02SACI 21999 December 11CLAin-flight failure
5VLS-1 V03SATEC2003CLApad explosion on 2003 August 22


Final schedule

[edit]

The V04 prototype was originally scheduled for launch in 2006. Further testing has resumed in 2008. The final VLS-1 schedule was as follows:[7]

#PhotoVehiclePayloadDatePlaceResult
1mockupelectrical tests with a mockup rocket[8][9]2012CLASuccess
2VLS-1 XVT-01 VSISNAVonly first two stages active2016CLAcanceled
3VLS-1 V-04satellite launch2018CLAcanceled

VLS Configurations

[edit]
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VLS-R1 test vehicle (1985)

[edit]

The VLS-R1 test vehicle had two stages, arranged in the following configuration:

  • Stage 1 - four S-20 rocket engines
  • Stage 2 - one dummy S-20 rocket engine

VLS-R2 test vehicle (1989)

[edit]

The VLS-R2 test vehicle had two stages, arranged in the following configuration:

  • Stage 1 - four S-20 rocket engines
  • Stage 2 - one S-20 rocket engine

VLS-XVI 01 sub-orbital test vehicle (2016, planned)

[edit]

The VLS-XVI 01 sub-orbital test vehicle has three solid fuel rocket stages and boosters, arranged in the following configuration:

VLS-1 operational configuration (2018, planned)

[edit]

The VLS-1 has three solid fuel rocket stages and boosters, arranged in the following configuration:

  • Stage 0 - four S-43 rocket engines
  • Stage 1 - one S-43TM rocket engine
  • Stage 2 - one S-40TM rocket engine
  • Stage 3 - one S-44 rocket engine

The rocket has four 400NRCS jets, located on the top of the third stage.

Developments

[edit]

VLM

[edit]
Main article:VLM (rocket)

TheVLM (Veículo Lançador de Microssatélites) based on theS50 rocket engine is being studied, with the objective of orbiting satellites up to 150 kg in circular orbits ranging from 250 to 700 km. It will be a three-stage rocket, expected to launch theSHEFEX III mission by theGerman Aerospace Center (DLR) in 2023.[10][11][12]

"Cruzeiro do Sul" (Southern Cross) program

[edit]

VLS Alfa

[edit]

In the framework of the proposedCruzeiro do Sul program,[13] the VLS-1 rocket is the basis of theVLS Alfa project.

L5 rocket based configuration - three-stage rocket, with the upper stage being liquid-fuel, putting 200 to 400 kg satellites into low equatorial orbits:

  • Stage 0 - four S-43 rocket engines
  • Stage 1 - one S-43TM rocket engine
  • Stage 2 - one S-40TM rocket engine
  • Stage 3 - one L5 rocket engine[7]

L75 rocket based configuration - two-stage rocket, with the upper stage being liquid-fuel, putting 500 kg satellites equatorial orbits up to 750 km:

  • Stage 0 - four S-43 rocket engines
  • Stage 1 - one S-43TM rocket engine
  • Stage 2 - one L75 rocket engine[7]
#PhotoVehiclePayloadDatePlaceResult
1VLS Alfa XVT-01-2015--
2VLS Alfa XVT-02-2016--
3VLS Alfa V-01-2017--
4VLS Alfa V-02SARA Orbital2018--
5VLS Alfa V-03-2020--

VLS Beta

[edit]

TheVLS Beta is another related project, intended to lift up to 800 kg payloads to an 800 km equatorial orbit. Its first flight was planned for 2020.[14][15]

Three-stage rocket, with the upper two stages being liquid-fuel.

  • Stage 1 - one P40 solid rocket engine
  • Stage 2 - one L300 rocket engines[16]
  • Stage 3 - one L75 rocket engine[7]

Projected flights are:[10]

#PhotoVehiclePayloadDatePlaceResult
1VLS Beta XVT-01-2018--
2VLS Beta XVT-02-2019--
3VLS Beta V-01-2020--

VLS Gama

[edit]

TheVLS Gama is intended to carry up to 1000 kg payloads to an 800 km polar orbit. Three-stage liquid-fuel rocket.

VLS Delta

[edit]

TheVLS Delta is capable of placing 2000 kg payloads in a geostationary orbit. Three-stage liquid-fuel rocket (VLS BETA body) with two solid fuel boosters.

VLS Epsilon

[edit]

TheVLS Epsilon is capable of placing 4000 kg payloads in a geostationary orbit. Three-stage liquid-fuel rocket (VLS BETA body) with two liquid-fuel boosters.

Gallery

[edit]
  • VLS-1 real size mockup
    VLS-1 real size mockup
  • Engine
    Engine
  • Engine test
    Engine test

See also

[edit]

References

[edit]
  1. ^ab"Problemas de "governança" e gestão explicam em parte extinção do VLS-1" [Problems with "governance" and management partly explain the extinction of the VLS-1.].jornaldosindct.sindct.org.br (in Portuguese). Archived fromthe original on 2016-08-16.
  2. ^"Veículo Lançador de Satélites (VLS)" [Satellite Launch Vehicle (VLS)] (in Portuguese). Brazilian Space Agency. Archived fromthe original on 2010-12-24. Retrieved2011-12-12.
  3. ^"CLA - Centro de Lançamento de Alcântara" [CLA - Alcântara Launch Center] (in Portuguese). Archived fromthe original on 2013-07-18. Retrieved2012-03-06.
  4. ^"Problemas de "Governança" e Gestão Explicam em Parte Extinção do VLS-1" ["Governance" and Management Problems Partly Explain the Extinction of the VLS-1] (in Portuguese).
  5. ^"Saiba como está o projeto Veículo Lançador de Satélite (VLS)" [Find out how the Satellite Launch Vehicle (VLS) project is progressing.].Brazilian Air Force (in Portuguese). Archived fromthe original on 2012-08-01. Retrieved2012-03-06.
  6. ^"VLS".space.skyrocket.de. Retrieved2016-05-07.
  7. ^abcd"Motor L5"(PDF).Espaço Brasileiro (in Portuguese) (12): 12. 2012.ISSN 1981-1187.
  8. ^Duarte, Leandro (2010)."Torre Móvel de Integração é concluida" [Mobile Integration Tower is completed.](PDF).Espaço Brasileiro (in Portuguese).10: 16.ISSN 1981-1187.
  9. ^"Brazil: IAE Conducts VLS Qualification Tests – Parabolic Arc". Archived fromthe original on 2012-04-10. Retrieved2012-04-20.
  10. ^ab"Brazilian space plans: from 2011 forward".forum.nasaspaceflight.com. Retrieved2012-03-06.
  11. ^"Brazilian Space".Brazilianspace.blogspot.com. Retrieved2011-12-12.
  12. ^"VLM: veículo lançador de microsatélites, launch vehicle for SHEFEX-3". German Aerospace Center (DLR). Archived fromthe original on 2014-09-03. Retrieved2013-05-24.
  13. ^"Instituto de Aeronáutica e Espaço" [Institute of Aeronautics and Space] (in Portuguese).Archived from the original on 2011-11-07. Retrieved2012-06-13.
  14. ^"Brasil planeja lançar foguetes ao espaço nos próximos anos; veja cronograma" [Brazil plans to launch rockets into space in the coming years; see the schedule.] (in Portuguese). Terra.
  15. ^"Acesso autônomo ao espaço - Onde o Brasil quer chegar" [Autonomous access to space - Where does Brazil want to go?] (in Portuguese). SindcCT. 22 May 2024.
  16. ^"VLS Beta".

External links

[edit]
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