Commant and Conquer Generals!

[Gast M16 Besitzer]

Ich mag es nicht Codename Panzers haut C & C Generals aus der Bahn glaubt mir.

[Master Chief 1]

Also die in der Webung haben gesagt das C & C Generäle einpacken können.

[Oberst_Klink 0]

Also die in der Webung haben gesagt das C & C Generäle einpacken können.

[Gast ::majoana::]

Also die in der Webung haben gesagt das C & C Generäle einpacken können.

[freaky 0]

In Generals geht es und 3 nationen die Krieg haben.

China, Usa und die IGB (Iraq).

[Gast M16 Besitzer]

Is ja auch egal

Wie man den abschaum nennen soll

Edit: Dürfen die überhaupt sagen das es C & C Generals weghaut?

Außerdem kann man die spiele überhaupt nich miteinander vergleichen.

[Gast M16 Besitzer]

Hier mal ne mod zum glotzen:

Bei der mod handelt sich es von der Cold War Crisis Mod. Sogar mit animirten piloten

[Geier 0]

Man kann schlecht spiele miteinander vergleichen, ausser sie handeln mit dem gleichen szenario und haben selbst das gleiche genre. In einzelnen Punkten kann man sie schon vergleichen aber nicht insgsamt. Ich find beide spiele geil

[Gast ::majoana::]

....Edit: Dürfen die überhaupt sagen das es C & C Generals weghaut?...

[Gast M16 Besitzer]

....Edit: Dürfen die überhaupt sagen das es C & C Generals weghaut?...

war das nciht sone bewertung von gamestar ?

geht die mod nur für zero hour oda auch nur für genearals.

aja:

Bei der mod handelt

[Gast M16 Besitzer]

Kann mir einer sagen was das ist?

[lookbehindyou 0]

The RT-21M / SS-20 is a solid-fuel, two-stage, theater-based ballistic missile based on the first and second stages of the SS-16. The SS-20 was probably intended to replace or augment the SS-4s and SS-5s deployed in the Soviet Eastern European theater, thus providing approximately three times the number of warheads of the older force.

The two-stage solid-fuel "Pioneer" with single-nozzle sustainers is derived from the first and second stages of the SS-16 ICBM. The cylindrical casings of the sustainer stages are made from composite materials. The solid propellant charge is rigidly fastened to the sustainer body.

The guidance/control system with its onboard digital computer and a gyro-stabilized platform with floating gyros enables the missile to be horizontally positioned and ensures optimal target accuracy. Flight control during the first stage flight is achieved through aerodynamic and jet vanes. During the second stage low temperature gas is injected into the diverging part of the sustainer nozzle.

The missile was deployed in a transport-launch canister, which was installed on a road-mobile launcher. The launcher was equipped with systems needed to ensure constant combat readiness, preparation and firing. The missile could be launched from a sliding roof garage at regimental bases or from field deployed sites. Before ignition the launcher was suspended on a hydraulic support, then the container was set upright in a vertical position. Before ignition of the first sustainer stage the missile was popped out of the container with the help of a solid propellant gas generator the missile and the first stage sustainer was started. The control of launch was conducted from a mobile control center. The SS-20 also has the capability to be reloaded and refired.

The developer of a complex was the Moscow institute of Thermal Technology which was headed by A.D. Nadiradzye. The flight-design tests were conducted from 21 September 1975 through 09 January 1976 at the Kapustin Yar test site. Deployment of the SS-20 began on 11 March 1976, and the first regiment equipped with the Pioneer missiles was set under airborne alert on 30 August 1976.

According to western data, the rocket was tested in three different Mods. The SS-20 Mod1&3 carried a single warhead whereas the SS-20 Mod2 carried a MIRV warhead. The Mod2 equipped with three warheads with a yield of 150 KT each became the standard missile. In this version the warheads are placed on a post-boost vehicle.

On 10 August 1979 the tests of the modernized "Pioneer"-UTTKh (15Zh53) began on the Kapustin Yar test site. They continued through 14 August 1980, and on 17 December 1980 the missile designated as SS-20 Mod3 was deployed. This variant had the same propulsion system as earlier versions, but it due to upgrading of a command structure and instrumentation-service unit it was possible to improve accuracy (CEP) from 550 to 450 meters, to increase maximum range by 10 %, and to increase the area covered by the warheads.

According to some Western assessments, with a new single, lightweight warhead, or with the addition of a third stage (or both), the SS-20 has the potential to be converted to an ICBM with limited capability against the continental United States.

Between 1978 throught 1986 a total of 441 launch complexes for the "Pioneer" missiles were deployed. The SS-20 was one of the missile systems eliminated under the terms of the INF Treaty, which took effect in June 1988. Prior to the INF drawdown, the SS-20 force comprised 48 bases that housed the regularly deployed force of 405 missiles and launchers.

The Intermediate-Range and Shorter-Range Nuclear Forces [iNF] Treaty was signed on 08 December 1987 and entered into force on 01 June 1988. The fundamental purpose of the INF Treaty was to eliminate and ban US and former USSR (FSU) ground-launched ballistic and cruise missiles, as well as associated support equipment, with ranges between 500 and 5500 kilometers. The first Soviet SS-20 missile and canister were eliminated under INF Treaty at the Kapustin Yar Missile Test Complex on 22 July 1988. The first Soviet SS-20 missiles were eliminated by launching at the Chita and Kansk missile sites on 25 August 1988. The last of 654 SS-20 missiles was eliminated at the Kapustin Yar Missile Test Complex on 12 May l991. And the last of 499 SS-20 launchers was eliminated at the Sarny Launcher Elimination Facility on 28 May 1991.

Specifications

Mod-1

Mod-2

Mod-3

DIA

SS-20

SS-20

SS-20/SS-X-28

NATO

Saber

Saber

Saber

Bilateral

RSD-10

RSD-10

RSD-10

Service

RSD-10/Pioneer

RSD-10/Pioneer-UTTX

RSD-10/Pioneer-3

OKB/Industry

15Zh45 (Temp-2C)

15Zh53 (Temp-2C)

15Zh53 (Temp-2C)

Design Bureau

Moscow Institute of Thermal Technology

Moscow Institute of Thermal Technology

Moscow Institute of Thermal Technology

Approved

3/4/1968

7/19/1977

8/14/1980

Years of R&D

Engineering and Testing

1974-76

1974-1976

1979-1980

First Flight Test

9/21/74

9/21/74

8/10/1979

IOC

1976

1976

1980

Deployment Date

3/11/1976

3/11/1976

12/17/1980

Type of Warhead

Single

MIRV

Single or MIRV

Warheads

1

3

1/3

Yield (Mt)

1.0

0.15

?

Payload (t)

1.5-1.74

1.5-1.74

?

Total length (m)

16.49

16.5

17.0

Total length w/o warhead (m)

14.9

14.9

14.9

Missile Diameter (m)

1.79

1.79

1.79

Launch Weight (t)

37

37

37

Fuel Weight (t)

Range (km)

600-5000

600-5000

600-5500/7500

CEP (m)

Russian Sources

0.550

0.550

0.450

CEP (m)

Western Sources

150-450

400-430`

?

Number of Stages

2

Canister length (m)

19.32

Canister length w/o front (m)

Canister diameter (m)

2.14

Booster guidance system

Inertial, autonomous

1st stage

2nd stage

2nd Stage

Length (m)

8.58

4.4-4.6

4.4-4.6

Body diameter (m)

1.79

1.47

1.47

Fueled weight (t)

26.7

8.63

8.63

Dry weight (t)

Solid Motor Designation

Design Bureau

Years R & D

Propellants

Solid

Solid

Solid

Fuel

N/A

N/A

N/A

Oxidizer

N/A

N/A

N/A

Burning time (sec.)

63

Thrust Sea Level/Vacuum (Tonnes)

Special Impulse (sec.)

Basing Mode

Ground mobile

Hardness

Launching Technique

Mortar Launch

Deployed boosters

0

Test Boosters

Warheads Deployed

0

Deployment Sites

INF Treaty data

Training Launchers

Space Booster Variant

N/A

[Gast ::majoana::]

ich denk dat is ne interkontinentalrakete (die rt21) also wohl ne mobile art. von den russen

guckst du Hier

?dit* ok das is für zh.

[lookbehindyou 0]

Hmm als Treibstoff kommt da unsymetrisches Dimethylhydrazin rein!

Lecker!

Leider habe ich jemandem ZH ausgeliehen und er will es mir nicht wiedergeben

[Gast ::majoana::]

unsymetrisches Dimethylhydrazin