Payload Launch Vehicle

from Wikipedia, the free encyclopedia
Launch of a PLV rocket with a prototype of the Exoatmospheric Kill Vehicle
Prototype of the Exoatmospheric Kill Vehicle

Payload Launch Vehicle (short PLV , dt. Payload launch carrier ) was a suborbital test rocket for the missile defense -Gefechtsköpfe the National Missile Defense .

construction

The PLV-rocket consists of the second (SR-19) and third stage (M-57a1) of disarmed Minuteman II - ICBM , identified by Lockheed Martin and the subcontractor Space Vector Corporation were converted. Instead of the Minuteman missile's original nuclear warhead, the PLV uses a kinetic warhead encased in a payload fairing. This warhead, known as the Exoatmospheric Kill Vehicle , is separated from the PLV missile outside the earth's atmosphere and maneuvers itself on a collision course with the approaching warhead.

All launches took place from a launch complex consisting of a missile silo on Meck Island in the Kwajalein Atoll. From 1997 to 2002 there were a total of ten starts, two of which were failures.

A new launch rocket, the OBV rocket, was developed for the operational ground-based interceptor system .

Similar missiles, also based on the combination of the SR-19 and M-57A1 stages of the Minuteman II missile, are the Hera target display missile modified by Coleman Aerospace and the SR-19 M-57A1 modified by Orbital Sciences Corporation .

Starts

No. Start date test success
1 June 23, 1997 IFT-1A
2 January 15, 1998 IFT-2
3 October 3, 1999 IFT-3
4th January 19, 2001 IFT-4
5 July 8, 2000 IFT-5 Partial success; Kinetic warhead is not disconnected
6th July 15, 2001 IFT-6
7th 4th December 2001 IFT-7
8th March 16, 2002 IFT-8
9 October 15, 2002 IFT-9
10 December 11, 2002 IFT-10 Partial success; Kinetic warhead is not disconnected

swell