![]() VS-40 rocket on display in Brazil  | |
| Function | Sounding rocket | 
|---|---|
| Country of origin | Brazil | 
| Size | |
| Height | 9.5 m (31 ft) | 
| Diameter | 1.01 m (3 ft 4 in) | 
| Mass | 6,800 kg (15,000 lb) | 
| Stages | 2 | 
| Capacity | |
| Payload to low Earth orbit | |
| Altitude | 650 km (400 mi) | 
| Mass | 500 kg (1,100 lb) | 
| Launch history | |
| Status | Active | 
| Launch sites | Alcântara Space Center, Andøya Space, Barreira do Inferno Launch Center | 
| Total launches | 3 | 
| Failure(s) | 1[1] | 
| First flight | 2 April 1993 | 
| First stage – S40TM | |
| Specific impulse | 275 seconds (2.70 km/s) | 
| Burn time | 56 seconds | 
| Second stage – S44M | |
| Maximum thrust | 33.24 kN (7,470 lbf) | 
| Specific impulse | 282 seconds (2.77 km/s) | 
| Burn time | 68 seconds | 
The VS-40 (Foguete Suborbital VS-40) is a Brazilian sounding rocket using solid fuel and stabilized aerodynamically.
The original version, VS-40, uses the S-40TM (4,200 kg) first stage engine and the S-44M (810 kg) second stage engine.[2][3][4] This configuration corresponds to the upper stages of the VLS-1 rocket.[5]
Version VS-40M used a S-40M engine for the first stage.[4]
Flights
VS40 performed the following flights:[4][6][7][8][9][10][1][11]
| Date | Version | Flight | Site | Mission | 
|---|---|---|---|---|
| 1993/04/02 | VS-40 | V01 | Alcântara | Operação Santa Maria - Qualifying flight for the S44 engine. 760 seconds in micro-gravity.[4] | 
| 1998/03/21 | VS-40 | V02 | Alcântara | Operação Livramento - VAP-1 (Fokker) payload.[12] | 
| 2012/06/22 | VS-40M | V03 | Andøya | SHEFEX (Sharp Edge Flight Experiment) II payload.[9][10] | 
| 2015/11/13 | VS-40M | Alcântara | Operação São Lourenço - SARA Suborbital 1 (reentry experiment) – Failure (exploded on pad) [6][7][8][1][12] | 
A flight of VS-40M carrying "SARA Suborbital 2" was planned but eventually cancelled. A future flight of VS-40M carrying HIFiRE 8 is in development.[4]
Characteristics

VS-40
- Length (mm) 6725
 - Payload Mass (kg) 500
 - Diameter (mm) 1000
 - Total takeoff mass (kg) 6,737
 - Mass of propellant (kg) 5,054
 - Structural mass (kg) 1,028
 - Apogee (km) 650
 - Microgravity time (s) 760
 
References
- 1 2 3 Brasileira, Força Aérea. "Projeto SARA continua, afirma Diretor de Ciência e Tecnologia Aeroespacial". Força Aérea Brasileira.
 - ↑ "O Foguete de sondagem VS-40". www.iae.cta.br. 2011. Archived from the original on 14 December 2011.
 - ↑ "VS-40". www.astronautix.com. Archived from the original on 3 March 2016.
 - 1 2 3 4 5 "S-40 Family". space.skyrocket.de.
 - ↑ "VS-40 - IAE". iae.dcta.mil.br. Retrieved 2023-12-03.
 - 1 2 "Projeto SARA". www.iae.cta.br. 2011. Archived from the original on 14 December 2011.
 - 1 2 "ANÁLISE DA ESTRUTURA INTERNA DO MÓDULO DE EXPERIMENTOS DO SARA SUBORBITAL" (PDF). www.inicepg.univap.br. 2008. Retrieved 2019-06-12.
 - 1 2 "Alcântara sedia encontro que discute atividade espacial no País". Governo do Brasil.
 - 1 2 "Sounding Rocket Campaigns « Andøya Rocket Range". Archived from the original on 2012-06-26. Retrieved 2012-06-26.
 - 1 2
 - ↑ "VS-40 - IAE". iae.dcta.mil.br. Retrieved 2023-12-03.
 - 1 2 Fan, Ricardo (2015-11-13). "FAB lança foguete VS-40 nesta sexta-feira". DefesaNet (in Brazilian Portuguese). Retrieved 2023-12-03.
 
External links
Wikimedia Commons has media related to VS-40.
- O Foguete de sondagem VS-40
 - Agência Espacial Brasileira :: Veículos Lançadores
 - SHEFEX 2 at Andoya Rocket Range
 
    This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.
