VLS-1 (original) (raw)
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
VLS-1
Brazilian all-solid orbital launch vehicle.
Status: Active. First Launch: 1997-11-02. Last Launch: 2003-08-22. Number: 3 . Payload: 120 kg (260 lb). Thrust: 1,172.00 kN (263,476 lbf). Gross mass: 50,700 kg (111,700 lb). Height: 19.50 m (63.90 ft). Diameter: 1.01 m (3.31 ft). Apogee: 750 km (460 mi).
4 stage vehicle consisting of 4 x S-43 + 1 x S-43TM + 1 x S-40TM + 1 x S-44.
LEO Payload: 120 kg (260 lb).
Family: all-solid, orbital launch vehicle. Country: Brazil. Spacecraft: SCD, SACI, SATEC, Unosat. Launch Sites: Alcantara, Alcantara VLS. Stages: S-43, S-44, S-40TM, S-43TM. Agency: INPE.
1997 November 2 - . 12:25 GMT - . Launch Site: Alcantara. Launch Complex: Alcantara VLS. LV Family: Sonda. Launch Vehicle: VLS-1. FAILURE: Destroyed during launch.. Failed Stage: 1.
- SCD-2A - . Mass: 115 kg (253 lb). Nation: Brazil. Agency: AEB. Manufacturer: INPE. Class: Technology. Type: Navigation technology satellite. Spacecraft: SCD. Apogee: 3.00 km (1.80 mi). The SCD-2A (Data Collection Satellite 2A) was a Brazilian satellite designed for the collection of meteorological data relayed by data collection platforms spread throughout the Brazilian territory..
1999 December 11 - . 18:25 GMT - . Launch Site: Alcantara. Launch Complex: Alcantara VLS. LV Family: Sonda. Launch Vehicle: VLS-1. FAILURE: Second stage failed to ignite; destroyed by range safety.. Failed Stage: 2.
- SACI-2 - . Mass: 80 kg (176 lb). Nation: Brazil. Agency: AEB. Manufacturer: INPE. Class: Technology. Type: Navigation technology satellite. Spacecraft: SACI. Apogee: 10 km (6 mi). Second attempted launch of Brazil's indigenous launcher..
2003 August 22 - . 16:30 GMT - . Launch Site: Alcantara. Launch Complex: Alcantara VLS. LV Family: Sonda. Launch Vehicle: VLS-1. FAILURE: Failure - Exploded on pad during final prelaunch processing. 21 people were killed, with none injured.. Failed Stage: 1.
- SATEC - . Payload: SATEC. Mass: 57 kg (125 lb). Nation: Brazil. Agency: INPE. Class: Technology. Type: Navigation technology satellite. Spacecraft: SATEC. COSPAR: F20030822A.
Launch was due on August 25. Was to have been on third qualification flight after two previous failures. The launch had already been delayed from October 2002, then May 7 and June 20 2003. It appeared that one of the strapon boosters ignited by accident. The two satellite payloads were also destroyed in the blast, as was the launch pad. - Unosat - . Payload: Unosat. Mass: 9.00 kg (19.80 lb). Nation: Brazil. Agency: Parana. Class: Technology. Type: Technology satellite. Spacecraft: Unosat. COSPAR: F20030822B.
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use