VLS-1 | |
| Function | Orbitallaunch vehicle |
|---|---|
| Manufacturer | CTA |
| Country of origin | Brazil |
| Size | |
| Height | 19.5 m (64 ft) |
| Diameter | 1.01 m (3.3 ft) |
| Mass | 50,700 kg (111,800 lb) |
| Stages | 3 |
| Capacity | |
| Payload tolow Earth orbit | |
| Mass | 380 kg (840 lb) |
| Launch history | |
| Status | Cancelled[1] |
| Launch sites | Alcântara VLS Pad |
| Total launches | 2 |
| Success(es) | 0 |
| Failure | 2 |
| Notable outcome | 1 (pad explosion in 2003) |
| First flight | 2 November 1997 (VLS-1 V01) |
| Last flight | 11 December 1999 (VLS-1 V02) |
| Boosters – S-43 | |
| No. boosters | 4 |
| Powered by | 1solid rocket booster |
| Total thrust | 303 kN (68,000 lbf) |
| Specific impulse | 225 s (2.21 km/s) |
| Burn time | 59 seconds |
| First stage – S-43TM | |
| Powered by | 1solid rocket booster |
| Specific impulse | 277 s (2.72 km/s) |
| Burn time | 58 seconds |
| Second stage –S-40TM | |
| Powered by | 1solid rocket booster |
| Specific impulse | 275 s (2.70 km/s) |
| Burn time | 56 seconds |
| Third stage –S-44 | |
| Powered by | 1solid rocket booster |
| Specific impulse | 282 s (2.77 km/s) |
| Burn time | 68 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]
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]
| # | Photo | Vehicle | Payload | Date | Place | Result |
|---|---|---|---|---|---|---|
| 1 | VLS-R1 | - | 1985 December 1 | CLA | Failure, apogee of 10 km. | |
| 2 | VLS-R2 | - | 1989 May 18 | CLA | Apogee of 50 km. | |
| 3 | VLS-1 V01 | SCD-2A | 1997 November 2 | CLA | in-flight failure | |
| 4 | VLS-1 V02 | SACI 2 | 1999 December 11 | CLA | in-flight failure | |
| 5 | VLS-1 V03 | SATEC | 2003 | CLA | pad explosion on 2003 August 22 |
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]
| # | Photo | Vehicle | Payload | Date | Place | Result |
|---|---|---|---|---|---|---|
| 1 | mockup | electrical tests with a mockup rocket[8][9] | 2012 | CLA | Success | |
| 2 | VLS-1 XVT-01 VSISNAV | only first two stages active | 2016 | CLA | canceled | |
| 3 | VLS-1 V-04 | satellite launch | 2018 | CLA | canceled |
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The VLS-R1 test vehicle had two stages, arranged in the following configuration:
The VLS-R2 test vehicle had two stages, arranged in the following configuration:
The VLS-XVI 01 sub-orbital test vehicle has three solid fuel rocket stages and boosters, arranged in the following configuration:
The VLS-1 has three solid fuel rocket stages and boosters, arranged in the following configuration:
The rocket has four 400NRCS jets, located on the top of the third stage.
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]
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:
L75 rocket based configuration - two-stage rocket, with the upper stage being liquid-fuel, putting 500 kg satellites equatorial orbits up to 750 km:
| # | Photo | Vehicle | Payload | Date | Place | Result |
|---|---|---|---|---|---|---|
| 1 | VLS Alfa XVT-01 | - | 2015 | - | - | |
| 2 | VLS Alfa XVT-02 | - | 2016 | - | - | |
| 3 | VLS Alfa V-01 | - | 2017 | - | - | |
| 4 | VLS Alfa V-02 | SARA Orbital | 2018 | - | - | |
| 5 | VLS Alfa V-03 | - | 2020 | - | - |
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.
Projected flights are:[10]
| # | Photo | Vehicle | Payload | Date | Place | Result |
|---|---|---|---|---|---|---|
| 1 | VLS Beta XVT-01 | - | 2018 | - | - | |
| 2 | VLS Beta XVT-02 | - | 2019 | - | - | |
| 3 | VLS Beta V-01 | - | 2020 | - | - |
TheVLS Gama is intended to carry up to 1000 kg payloads to an 800 km polar orbit. Three-stage liquid-fuel rocket.
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.
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.