Palmachim Base de Misiles intercontinentales de Israel

Palmachim Base de Misiles intercontinentales de Israel
PARA: 1
Palmachim
Credit: © Mark Wade



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Tipo: Sitio de lanzamiento Orbital. Operador: Israel. País: Israel. Latitud: 31 ° 54 N. longitud: 34 ° 42 e. mínima inclinación: 142.0 grados. Inclinación máxima: 144,0 grados. Comentarios: Sitio de Misiles israelíes y el sitio desde el cual se lanza también Vehiculo Orbital Shavit . Un lanzamiento debido a oeste sobre el Mediterráneo es necesario para evitar que sobrevolaba los países árabes, resultando en la dirección y la inclinación orbital único.
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Launch Pads
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•Sea Launch Area Latitude: 31.9000 N. Longitude: 34.6000 E. Launch Pads: 1. First Launch: 1990-08-09. Last Launch: 1999-11-01. Number launches: 14. Arrow 1.

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Palmachim Chronology and Launch Log

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May 1987 - Jericho 2. Apogee: 300 km.
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1988 Sep 19 9:32 - Shavit. Shaviyt 1
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1989 Sep 14 - Jericho 2. Apogee: 300 km.
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1990 Apr 3 12:02 - Shavit. Shaviyt 2
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1990 Aug 9 - Arrow 1. Failure. LC: Israeli ship. Apogee: 0.000 km. Launched from Israeli vessel.
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1991 Mar 25 - Arrow 1. LC: Israeli ship. Apogee: 20 km. Launched from Israeli vessel.
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1991 Oct 30 - Arrow 1. LC: Israeli ship. Apogee: 20 km. Launched from Israeli vessel.
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1992 Sep 23 - Arrow 1. LC: Israeli ship. Apogee: 20 km. Launched from Israeli vessel.
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1993 Feb 28 - Arrow 1. LC: Israeli ship. Apogee: 20 km. Launched from Israeli vessel.
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1993 Feb 28 - Arrow 1. LC: Israeli ship. Apogee: 20 km. Launched from Israeli vessel.
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1993 Jul 14 - Arrow 1. LC: Israeli ship. Apogee: 20 km. Launched from Israeli vessel.
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1993 Oct 14 - Arrow 1. LC: Israeli ship. Apogee: 20 km. Launched from Israeli vessel.
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1993 Oct 14 - Arrow 1. LC: Israeli ship. Apogee: 20 km. Launched from Israeli vessel.
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March 1994 - Arrow 1. LC: Israeli ship. Apogee: 20 km. Launched from Israeli vessel.
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1994 Jun 12 - Arrow 1. LC: Israeli ship. Apogee: 20 km. Launched from Israeli vessel.
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1994 Sep 15 - Ofeq Shavit. Failure not acknowledged..
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1994 Sep 15 - Jericho II 3? Jericho 2. Apogee: 300 km. 'Ofeq?
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1995 Apr 5 11:16 - Shavit 1. Shaviyt 1 3
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1995 Jul 30 - Arrow 2 F1 Arrow 2. Apogee: 20 km.
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1996 Feb 20 - Arrow 2 F2 Arrow 2. Apogee: 80 km.
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1996 Aug 20 - Arrow 1. LC: Israeli ship. Apogee: 80 km. Launched from Israeli vessel.
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1996 Aug 20 - Arrow 2 F3 Arrow 2. Apogee: 80 km.
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1997 Mar 11 - Arrow 2 F4 Arrow 2. Apogee: 80 km.
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August 1997 - Arrow 1. LC: Israeli ship. Apogee: 80 km. Launched from Israeli vessel.
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August 1997 - Arrow 2 F5 Arrow 2. Apogee: 80 km.
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1998 Jan 22 12:56 - Shavit 1. Launch vehicle failed during second stage burn.. Shaviyt 1 4
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1998 Sep 14 12:41 - Arrow 2 F6 Arrow 2. Apogee: 80 km.
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1999 Nov 1 9:42 - Arrow 2 F7 Arrow 2. Apogee: 80 km.
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1999 Nov 1 9:42 - Arrow 1 TM-91 Arrow 1. LC: Israeli ship. Apogee: 80 km. Launched from Israeli vessel.
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2000 Sep 14 - Arrow 2 F8 Arrow 2. Apogee: 80 km.
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2001 Jun 27 - Jericho 2. Apogee: 100 km.
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2001 Aug 27 10:50 - Arrow 2. Apogee: 100 km.
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2002 May 28 15:25 - Shavit 1. Shaviyt 1 5
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Bibliography:

•McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Web Address when accessed: http://hea-www.harvard.edu/~jcm/space/space.html.