MABES

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

MABES

MABES
Credit: Manufacturer Image

Japanese technology satellite. MABES (Jindai). Experiment on the levitation of the magnetic bearing flywheel under zero-g condition. Technology satellite operated by NASDA, Japan. Launched 1986.

AKA: Jindai. Status: Operational 1986. First Launch: 1986-08-12. Last Launch: 1986-08-12. Number: 1 .

More at: MABES.

Family: Medium earth orbit, Technology, Technology satellite. Country: Japan. Launch Vehicles: Thor, Delta, H-1. Launch Sites: Tanegashima, Tanegashima N. Agency: NASDA. Bibliography: 2, 279, 6.

1986 August 12 - . 20:45 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima N. LV Family: Thor. Launch Vehicle: H-1.

MABES - . Payload: Jindai/LE-5. Nation: Japan. Agency: NASDA. Class: Technology. Type: Navigation technology satellite. Spacecraft: MABES. USAF Sat Cat: 16910 . COSPAR: 1986-061C. Apogee: 1,604 km (996 mi). Perigee: 1,483 km (921 mi). Inclination: 50.00 deg. Period: 117.00 min. MABES (Jindai). Experiment on the levitation of the magnetic bearing flywheel under zero-g condition. .

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