cosmos.wikisort.org - SpacecraftCerise (French for "cherry") was a French military reconnaissance satellite. Its main purpose was to intercept HF radio signals for French intelligence services.[1] With a mass of 50 kg, it was launched by an Ariane rocket from Kourou in French Guiana at 17:23 UT, 7 July 1995.[1] Cerise's initial orbital parameters were period 98.1 min, apogee 675 km, perigee 666 km, and inclination 98.0 deg.[1]
Cerise Illustration of debris colliding with Cerise |
|
| Mission type | Military reconnaissance |
|---|
| COSPAR ID | 1995-033B  |
|---|
| SATCAT no. | 23606 |
|---|
|
|
|
|
| Bus | SSTL-70 |
|---|
| Manufacturer | Alcatel Space · Surrey Satellite Technology |
|---|
| Launch mass | 50 kg (110 lb) |
|---|
| Dry mass | 50kg |
|---|
| Dimensions | 0.6 × 0.3 × 0.3 m (1.97 × 0.98 × 0.98 ft) |
|---|
|
|
|
|
| Launch date | 7 July 1995, 16:23:34 (1995-07-07UTC16:23:34) UTC |
|---|
| Rocket | Ariane 4 V-75 |
|---|
| Launch site | Guiana Space Centre ELA-2 |
|---|
| Contractor | Arianespace |
|---|
|
|
|
|
| Reference system | Geocentric |
|---|
| Regime | Sun-synchronous |
|---|
| Eccentricity | 0.0005756 |
|---|
| Perigee altitude | 581 km (361 mi) |
|---|
| Apogee altitude | 589 km (366 mi) |
|---|
| Inclination | 98.2413° |
|---|
| Mean motion | 14.94 rev/day |
|---|
| Epoch | 27 December 2016 12:15:03 UTC |
|---|
|
|
| |
On 24 July 1996 it was hit by a catalogued space debris object from an Ariane rocket, making it the first verified case of an accidental collision between two artificial objects in space.[2][3]
The collision (with relative velocity of 14.8 km/s) tore off a 2.8-2.9 metre (9.2-9.5 foot) portion of Cerise's gravity-gradient stabilization boom, which left the satellite severely damaged and tumbling with a limited attitude control system. Novel magnetic control algorithms were used to re-stabilise the otherwise undamaged microsatellite to regain almost full operational mission capability.[4][5]
See also
Spaceflight portal
References
External links
Earth reconnaissance satellites (excluding Russia and the United States) |
|---|
China  | | IMINT |
- JSSW
- FSW-0
- FSW-1
- FSW-2
- FSW-3
- JianBing
|
|---|
| SIGINT | |
|---|
|
|---|
France  | |
|---|
Germany  | |
|---|
India  | |
|---|
Israel  | |
|---|
Italy  | |
|---|
Japan  | | IMINT |
- IGS 1A/B
- IGS 2A/B
- IGS 3A
- IGS 4A/B
- IGS 5A
- IGS 6A
- IGS 7A
- IGS 8A/B
|
|---|
|
|---|
South Korea  | |
|---|
Spain  | |
|---|
Turkey  | |
|---|
United Kingdom  | |
|---|
← 1994 · Orbital launches in 1995 · 1996 → |
|---|
|
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |
Текст в блоке "Читать" взят с сайта "Википедия" и доступен по лицензии Creative Commons Attribution-ShareAlike; в отдельных случаях могут действовать дополнительные условия.
Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
2019-2026
WikiSort.org - проект по пересортировке и дополнению контента Википедии