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Alfa MRBM
Total mass: 8,000
kg
Warhead: 1,000 kg
Maximum range: 1000 km
Ceiling: 300 km
First launch: 1976 |
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| SXB 3 |
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SXB 3
Engines:
0. 2 × dummy boosters
1. 1 × P9.5 | PAP-14 |
 |
Launches: 1 (Failures: 0)
/1992/
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Retired |
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| |
 |
Engines:
0. 2 × P9.5 | PAP
1. 1 × Algol-3A
2. 1 × Castor-2A
3. 1 × Antares-3A
4. 1 × Mage-2
Total mass: 46,0000
kg
Payload (LEO): 520 kg
Status: Cancelled |
 |
Never flown |
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| |
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Engines:
0. 4 × P9.5 | PAP
1. 1 × P9.5 | PAP
2. 1 × Castor-2A
3. 1 × Antares-3A
4. 1 × Mage-2
Total mass: 70,0000
kg
Status: Cancelled |
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Never flown |
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| VLS |
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VLS-1
Engines:
1. 4 × S-43
2. 1 × S-43TM
3. 1 × S-40TM
4. 1 × S-44
Total mass: 49,950
kg
Payload:
(LEO)
(LPEO)
(SSO) |
380 kg
250 kg
80 kg |
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Launches: 3 (Failures: 3)
/1997-2003/
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Payload: SCD, SACI, SATEC, UNOSAT |
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Retired |
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Engines:
1. 4 × S-43
2. 1 × S-43TM
3. 1 × S-40TM
1. 1 × MFPL-15
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Never flown |
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| Spectrum |
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Spectrum
Engines:
9. 1 × Aquila-SL
1. 1 × Aquila-Vac
Total mass: 49,950
kg
Payload:
(LEO)
(SSO) |
1,000 kg
700 kg |
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Launches: 1 (Failures: 1)
/2025/
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In service |
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| Eris Block 1 |
 |
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Launches: 1 (Failures: 1)
/2025/
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In service |
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Al-Samoud 1
Engines:
1. 1 × S2.720
Apogee: 50 km
First launch: 1997 |
|
Al-Samoud 2
Engines:
1. 1 × S2.720
Apogee: 45 km
First launch: 2001 |
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Al Hussein
(Scud-B)
Engines:
1. 1 × S 5.2
Total mass: 6,800 kg
Maximum range: 650 km
Apogee: 85 km
Warhead: 250
kg
First launch: 1987
Operational Capability: 1988 |
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Al Hijara
First launch: 1990 |
|
Al Abbas
Engines:
1. 1 × S 5.2
Total mass: 7,700 kg
Maximum range: 800
km
Warhead: 125
kg
First launch: 1988 | |
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| Al Abid |
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Al Abid
Engines:
1. 5 × S 5.2
2. none
1 × S 5.2 (unflown)
1 × S 5.2 (unflown)
Payload (LEO): 100-300 kg
Total mass: 48,000 kg |
|
Launches: 1 (Failures: 1)
/1989/
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Retired |
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Burkan-1
(Scud-B)
Engines:
1. 1 × S 5.2
Total mass: 7,300 kg
Maximum range: 800 km
Warhead: 500 kg
First launch: 2016
Operational Capability:: 2016 |
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Burkan-2
Scud-C)
Engines:
1. 1 × S 5.2 | |
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Al Zafer
Engines:
1. 1 × LRBA
Maximum range: 376 km |
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Al Kaher-3
Engines:
1. 1 × Model 39
Total mass: 10,000 kg
Maximum range: 500 km
Warhead: 1000
kg | |
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Ghauri-1
(Nodong)
Engines:
1. 1 × Nodong
Total mass: 14,500 kg
Apogee: 150 km
Maximum range: 1,200 km
Warhead: 700
First launch: 1998 |
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Ghauri-2
(Nodong+)
Engines:
1. 1 × Nodong+ |
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Ghaznavi
Engines:
1. 1 × |
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Shaheen-1
Engines:
1. 1 ×
2. 1 ×
Total mass: 6,200 kg
Maximum range: 750 km
Apogee: 100 km
Warhead: 950
kg
First launch: 1999
Operational Capability: 2003 |
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|
Shaheen-2
(
Hatf-6)
Engines:
1. 1 ×
2. 1 ×
Total mass: 23,600 kg
Maximum range: 2,500 km
Apogee: 300 km
Warhead: 1,230 kg / 40 kT
Operational Capability: 2014 |
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Shaheen-3
Engines:
1. 1 ×
2. 1 ×
Maximum range: 3,000 km
Warhead: 50 kT |
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| Taimoor |
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Ababeel
(Taimoor)
Engines:
1. 1 × L-SpaB-140
2. 1 ×
3. 1 ×
4. 1 ×
Total mass: 34.500 kg
Payload:
(SSO) 300 kg |
|
aunches: 2 (Failures: 2)
/2017-2018/
|
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In service |
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SORS
Engines:
1. 1 × SORS |
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Never flown |
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