INTA-255
The INTA-255 was a Spanish sounding rocket developed by the Instituto Nacional de Tecnica Aerospacial.
Manufacturer | INTA |
---|---|
Country of origin | Spain |
Size | |
Height | 6.03 m |
Diameter | 26 cm |
Mass | 340 kg |
Stages | 2 |
Capacity | |
Payload to Suborbital | |
Altitude | 150 km |
Mass | 15 kg (33 lb) |
Associated rockets | |
Derivative work | INTA-300 |
Launch history | |
Status | Retired |
Launch sites | El Arenosillo |
Total launches | 3 |
Success(es) | 3 |
Failure(s) | 0 |
It was based on existing british solid rocket motors: four Chick rockets as a booster stage and a single Goose-2 as stage 1. All the engines were fired at launch, with the Chicks burning for 0.2 seconds and the Goose-2 continuing for 17 seconds.
The apogee of INTA-255 was 150 km for a 5 kg payload, the takeoff thrust 42.00 kN, the gross mass 340 kg, the diameter 0.26 m and the length to 6.03 m.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.