VSB-30
Function | Sounding rocket |
---|---|
Manufacturer | Institute of Aeronautics and Space |
Country of origin | Brazil |
Size | |
Height | 12,6 m |
Diameter | 0.56 m |
Mass | 2,570 kg |
Stages | 2 |
Capacity | |
Payload to Suborbital (270 km) | |
Mass | 400 kg |
Launch history | |
Status | Active |
Launch sites | Alcântara Esrange |
First flight | 2004 October 23 |
First stage - S-31 | |
Engines | 1 Solid |
Thrust | 240.00 kN |
Burn time | 11 seconds |
Propellant | Solid |
Second stage S-30 | |
Engines | 1 Solid |
Thrust | 102.00 kN |
Burn time | 20 seconds |
Propellant | Solid |
VSB-30 - "Veículo de Sondagem Booster – 30" (Booster Sounding Vehicle) or "Foguete Suborbital VSB-30" is the designation of a Brazilian sounding rocket, which replaced the Skylark rocket at Esrange.
The VSB-30 is based on the VS-30 rocket (S-30 engine) with the addition of a booster stage (S-31 engine). Development started in 2000 in cooperation with DLR.[1] The rocket can carry a payload of 400 kg to an altitude of 270 km.[1] It has a liftoff thrust of 240 kN and a total mass of 2570 kg. It has a diameter of 0.56 m and a length of 12.6 m.
VSB-30 was first launched on October 23, 2004, at Alcântara Launch Center. The first launch at Esrange took place on December 1, 2005.
Flights
VSB-30 performed the following flights:[2][3][4]
Date | Flight | Site | Name | Apogee |
---|---|---|---|---|
2004 October 23 | XV-01 | Alcântara | Cajuana test | 240 km |
2005 December 1 | V02 | Esrange | TEXUS EML-1/TEXUS 42 Microgravity mission | 263 km |
2006 May 10 | V03 | Esrange | TEXUS 43 Microgravity mission | 237 km |
2007 July 19 | V04 | Alcântara | Cuma II Microgravity mission | 242 km |
2008 February 7 | V05 | Esrange | DLR TEXUS 44 (EML-2) | 264 km |
2008 February 21 | V06 | Esrange | DLR TEXUS 45 | 270 km |
2008 May 15 | V08 | Esrange | MASER 11 | 252 km |
2009 November 22 | V09 | Esrange | TEXUS 46 | |
2009 November 29 | V10 | Esrange | TEXUS 47 | |
2010 December 12 | V07 | Alcântara | MICROG 1A | 242 km |
2011 March 29 | V15 | Esrange | TEXUS 49 | 268 km |
2011 March 29 | V14 | Esrange | TEXUS 48 | 268 km |
2012 February 13 | V16 | Esrange | MASER 12[5] | 259 km[5] |
2013 April 12 | V17 | Esrange | TEXUS 50 | |
2015 February 22 | V20 | Esrange | CRYOFENIX | |
2015 March 30 | V13 | Andøya | HIFiRE 7 | |
2015 April 23 | V18 | Esrange | TEXUS 51 | |
2015 April 27 | V21 | Esrange | TEXUS 52 | |
2015 July 30 | V24 | Esrange | Mapheus 5 | |
2015 December 1 | V22 | Esrange | MASER 13 | |
2016 January 23 | V23 | Esrange | TEXUS 53 | |
2016 December 7 | V11 | Alcântara | MICROG 2 | |
2017 January 23 | V19 | Esrange | MAIUS 1 | |
2017 May 13 | V24 | Esrange | MAPHEUS 6 | |
2017 June 30 | V12 | Woomera | HIFiRE 4a / HIFiRE 4b | |
2018 May 13 | V26 | Esrange | TEXUS 54 | |
2018 May 31 | V27 | Esrange | TEXUS 55 | |
2019 June 24 | V?? | Esrange | MASER-14 | 260 km |
2019 November 15 | V?? | Esrange | TEXUS-56 | 256 km |
2021 December 14 | V32 | Alcântara | Cruzeiro Operation (14-X S)[6] | 280 km[6] |
2022 October 1 | V?? | Esrange | TEXUS-57 | |
2022 October 23 | V29 | Alcântara | Operação Santa Branca (MQ-PSM) | 227 km |
2022 November 23 | V?? | Esrange | S1X-3/MASER 15 (SubOrbital Express 3) | 260 km |
2023 April 24 | V?? | Esrange | TEXUS-58 | 250 km |
2023 December 2 | V?? | Esrange | MAIUS-2 |
Characteristics
VSB-30 has the following configuration:
- Length (mm): 12600
- Stages: 2
- Payload Mass (kg): 400
- Diameter (mm): 570
- Total takeoff mass (kg): 2570
- Apogee (Max km): 270
Stages
S-30 solid rocket stage
- Gross Mass: 1,200 kg (2,646 lb)
- Unfuelled mass: 341 kg (752 lb)
- Height: 3.30 m (10.80 ft)
- Diameter: 0.56 m (1.83 ft)
- Thrust: 102.00 kN (22,930 lbf)
- Burn time: 20 s
S-31 solid rocket stage
- Gross Mass: 900 kg (1,984 lb)
- Unfuelled mass: 284 kg (626 lb)
- Height: 3.20 m (10.40 ft)
- Diameter: 0.56 m (1.83 ft)
- Thrust: 240.00 kN (53,950 lbf)
- Burn time: 11 s
See also
References
- ^ a b "VSB-30 - IAE". iae.dcta.mil.br. Retrieved 2023-12-03.
- ^ "VSB-30". Archived from the original on 2015-08-24. Retrieved 2015-08-05.
- ^ "S-30 family". space.skyrocket.de.
- ^ "VSB-30". Gunter's Space Page. Retrieved 2023-12-03.
- ^ a b "IAE Lança Com Sucesso Mais um Foguete VSB-30".
- ^ a b "FAB realiza primeiro teste de voo do motor aeronáutico hipersônico 14-X - Força Aérea Brasileira". www.fab.mil.br. Retrieved 2022-04-15.
External links
- History of Brazilian space launchers: VSB-30 (in Portuguese)
- Space Agency of Brazil: VSB-30 (in Portuguese)