To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

From Wikipedia, the free encyclopedia

VS-40 (Foguete Suborbital VS-40)
Foguete VS 40.jpg
VS-40 rocket on display in Brasília
FunctionSounding rocket
ManufacturerInstituto de Aeronáutica e Espaço
Country of originBrazil
Size
Height9.50 m (31.10 ft)
Diameter1.01 m (3.31 ft)
Mass6,800 kg (14,900 lb)
Stages2
Capacity
Payload to LEO500 kg (650 km)
Launch history
StatusActive
Launch sitesCentro de Lançamento de Alcântara, Andøya Rocket Range, Centro de Lançamento da Barreira do Inferno
Total launches3
Failure(s)1[1]
First flight2 April 1993
First stage - S40TM
Engines1 Solid
Thrust208.39 kN (46,848 lbf)
Specific impulse275 s (2.70 kN·s/kg)
Burn time56 seconds
PropellantSolid
Second stage S44M
Engines1 Solid
Thrust33.24 kN
Specific impulse282 s
Burn time68 seconds
PropellantSolid

The VS-40 (Foguete Suborbital VS-40) is a Brazilian sounding rocket using solid fuel, stabilized aerodynamically, distributed between the first stage S40TM (4,200 kg) engine and the second stage S44M (810 kg) engine.[2][3] This configuration corresponds to the upper stages of the VLS-1 rocket.

Flights[4]

Characteristics

VS-40
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. ^ a b Brasileira, Força Aérea. "Projeto SARA continua, afirma Diretor de Ciência e Tecnologia Aeroespacial". Força Aérea Brasileira.
  2. ^ "IAE - Página inicial". www.iae.cta.br.
  3. ^ "Encyclopedia Astronautica Index: 1". www.astronautix.com.
  4. ^ a b "S-40 Family". space.skyrocket.de.
  5. ^ "Archived copy". Archived from the original on 2012-06-26. Retrieved 2012-06-26.CS1 maint: archived copy as title (link)
  6. ^ [1][dead link]
  7. ^ "IAE - Página inicial". www.iae.cta.br.
  8. ^ "ANÁLISE DA ESTRUTURA INTERNA DO MÓDULO DE EXPERIMENTOS DO SARA SUBORBITAL" (PDF). www.inicepg.univap.br. 2008. Retrieved 2019-06-12.
  9. ^ "Alcântara sedia encontro que discute atividade espacial no País". Governo do Brasil.

External links

This page was last edited on 19 September 2019, at 20:41
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.