Bélier (rocket)

{{Short description|French sounding rocket}}

File:Belier Musee du Bourget 2.JPG]]

File:Sudav-belier.gif

File:Sudav-belier-family.gif

Bélier is the designation of a French sounding rocket family.{{Cite web |title=Belier |url=https://space.skyrocket.de/doc_lau/belier.htm |access-date=2023-07-30 |website=Gunter's Space Page |language=en}}{{Cite web |title=Belier |url=http://www.astronautix.com/b/belier.html |access-date=2023-08-14 |website=www.astronautix.com}} Three versions of the Bélier were launched between 1961 and 1970 at the CIEES launch facility at Hammaguir, the Salto di Quirra and Ile du Levant missile ranges, and Kourou Space Center.{{Cite web |title=Belier I |url=http://www.astronautix.com/b/belieri.html |access-date=2023-08-14 |website=www.astronautix.com}}{{Cite web |title=Belier II |url=http://www.astronautix.com/b/belierii.html |access-date=2023-08-14 |website=www.astronautix.com}}{{Cite web |title=Belier III |url=http://www.astronautix.com/b/belieriii.html |access-date=2023-08-14 |website=www.astronautix.com}}

After its retirement, the Bélier was used as a stage for a family of solid-propellant rockets, including the Centaure, the Dragon, the Dauphin and the Éridan.{{Cite web |title=Dragon |url=https://space.skyrocket.de/doc_lau/dragon.htm |access-date=2023-07-30 |website=Gunter's Space Page |language=en}}{{Cite web |title=Centaure |url=https://space.skyrocket.de/doc_lau/centaure.htm |access-date=2023-07-30 |website=Gunter's Space Page |language=en}}

Versions

= Belier I =

The first Belier single stage rocket, powered by a Jericho motor.

  • payload: 30 kg
  • apogee: 80 km
  • takeoff thrust: 20.00 kN
  • takeoff weight: 313 kg
  • diameter: 0.31 m
  • length: 4.01 m
  • fin span: 0.78 m

= Belier II =

Upgraded Belier single stage rocket, using 'Plastolite' propellant.

  • payload: 30 kg
  • apogee: 130 km
  • takeoff thrust: 21.50 kN
  • takeoff weight: 352 kg
  • diameter: 0.31 m
  • length: 5.90 m
  • fin span: 0.78 m

= Belier III =

Upgraded Belier single stage rocket, powered by a Vega motor using 'Isolane' propellant.

  • apogee: 109 km
  • takeoff weight: 400 kg
  • diameter: 0.31 m
  • length: 3.80 m

Belier III launches:

class="wikitable sortable"

!Date

!Launch Site

!Nation

!Agency

!Apogee (km)

!Mission

1968 March 18

|Biscarrose

|France

|CNES

|0

|{{Failure}}

1968 May 14

|Salto di Quirra

|Europe

|CNES, ESRO

|130

|Test mission

1969 March 6

|Kourou Space Center

|France

|CNES

|100

|Test mission

1969 September 25

|Biscarrose

|France

|ONERA

|60

|CRAPEL/ELECTRE re-entry vehicle test flight

{{Commonscat|Belier (rocket)}}

See also

References