Misplaced Pages

VS-40

Article snapshot taken from Wikipedia with creative commons attribution-sharealike license. Give it a read and then ask your questions in the chat. We can research this topic together.
VS-40 (Foguete Suborbital VS-40)
VS-40 rocket on display in Brazil
FunctionSounding rocket
Country of originBrazil
Size
Height9.5 m (31 ft)
Diameter1.01 m (3 ft 4 in)
Mass6,800 kg (15,000 lb)
Stages2
Capacity
Payload to sub-orbital flight
Altitude650 km (400 mi)
Mass500 kg (1,100 lb)
Launch history
StatusActive
Launch sitesAlcântara Space Center, Andøya Space, Barreira do Inferno Launch Center
Total launches3
Failure(s)1
First flight2 April 1993
First stage – S40TM
Gross mass4,200 kg (9,300 lb)
Specific impulse275 seconds (2.70 km/s)
Burn time56 seconds
Second stage – S44M
Gross mass810 kg (1,790 lb)
Maximum thrust33.24 kN (7,470 lbf)
Specific impulse282 seconds (2.77 km/s)
Burn time68 seconds
[edit on Wikidata]

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. This configuration corresponds to the upper stages of the VLS-1 rocket.

Version VS-40M used a S-40M engine for the first stage.

Flights

VS40 performed the following flights:

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.
1998/03/21 VS-40 V02 Alcântara Operação Livramento - VAP-1 (Fokker) payload.
2012/06/22 VS-40M V03 Andøya SHEFEX (Sharp Edge Flight Experiment) II payload.
2015/11/13 VS-40M Alcântara Operação São Lourenço - SARA Suborbital 1 (reentry experiment) – Failure (exploded on pad)

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.

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. ^ Brasileira, Força Aérea. "Projeto SARA continua, afirma Diretor de Ciência e Tecnologia Aeroespacial". Força Aérea Brasileira.
  2. "O Foguete de sondagem VS-40". www.iae.cta.br. 2011. Archived from the original on 14 December 2011.
  3. "VS-40". www.astronautix.com. Archived from the original on 3 March 2016.
  4. ^ "S-40 Family". space.skyrocket.de.
  5. "VS-40 - IAE". iae.dcta.mil.br. Retrieved 2023-12-03.
  6. ^ "Projeto SARA". www.iae.cta.br. 2011. Archived from the original on 14 December 2011.
  7. ^ "ANÁLISE DA ESTRUTURA INTERNA DO MÓDULO DE EXPERIMENTOS DO SARA SUBORBITAL" (PDF). www.inicepg.univap.br. 2008. Retrieved 2019-06-12.
  8. ^ "Alcântara sedia encontro que discute atividade espacial no País". Governo do Brasil.
  9. ^ "Sounding Rocket Campaigns « Andøya Rocket Range". Archived from the original on 2012-06-26. Retrieved 2012-06-26.
  10. ^
  11. "VS-40 - IAE". iae.dcta.mil.br. Retrieved 2023-12-03.
  12. ^ Fan, Ricardo (2015-11-13). "FAB lança foguete VS-40 nesta sexta-feira". DefesaNet (in Brazilian Portuguese). Retrieved 2023-12-03.

External links

Brazil Brazilian space program
Science and technology in Brazil
Satellites
Programs
In development
Sounding
rockets
Active
Canceled
Launch
vehicles
In development
Canceled
  • VLS-1 ("Cruzeiro do Sul" launcher family)
  • Tsyklon-4 (collaboration with Ukraine)
Launch sites
Organisation
Missions
International programs


Stub icon

This rocketry article is a stub. You can help Misplaced Pages by expanding it.

Categories: