Japanese technology satellite. One launch, 1976.02.04. Japanese technology satellite.
Gross mass: 92 kg (202 lb).
First Launch: 1976.02.04.
Number: 1 .
More... - Chronology...
Associated Countries
See also
-
Mu The Japanese Mu launcher series provided a flexible all-solid propellant launch vehicle for access to space. It was the first Japanese launch vehicle designed from the start as an orbital launch vehicle. More...
Associated Launch Vehicles
-
Mu The Japanese Mu launcher series provided a flexible all-solid propellant launch vehicle for access to space. It was the first Japanese launch vehicle designed from the start as an orbital launch vehicle. More...
-
Mu-3C Japanese all-solid orbital launch vehicle. Four stage vehicle consisting of 8 x SB-310 + 1 x M-10 + 1 x M-22TVC + 1 x M-3A More...
-
Mu-3 The Japanese Mu launcher series provided a flexible all-solid propellant launch vehicle for access to space. More...
Bibliography
-
Bramscher, Robert G, "A Survey of Launch Vehicle Failures", Spaceflight, 1980, Volume 22, page 351.
Associated Launch Sites
-
Kagoshima Japanese launch center for solid fueled sounding rockets and satellite launchers. Limited to two months a year due to disturbance of local fisheries. More...
Corsa A Chronology
1976 February 4 - .
Launch Site:
Kagoshima.
Launch Complex:
Kagoshima M.
LV Family:
Mu.
Launch Vehicle:
Mu-3C.
LV Configuration: Mu-3C M-3C-3.
FAILURE: Stage 2 thrust vector control failure..
Failed Stage: 2.
- Corsa A - .
Mass: 92 kg (202 lb). Nation: Japan. Agency: ISAS. Class: Technology. Type: Navigation technology satellite. Spacecraft: Corsa A. Decay Date: 1976-02-04 . COSPAR: F760204A.
Home - Browse - Contact
© / Conditions for Use
