RudraM Series Air-launched Missiles : Updates & Discussions

Are we going to induct the RudraM-I?
We probably will if we aren't already. A 100-150 km range missile it isn't exactly a short-range missile. The range just looks less impressive, compared to the other missiles.

What the M-1 lacks in range is made up for with unit cost. This is especially true as stealthy armed wingman drones comes to the scene. The other missiles are too heavy to be fired from a wingman drone. Deploying a M-1 missile from a wingman will always cost less than deploying a M-2 or M-3 from a heavy fighter.
 
We probably will if we aren't already. A 100-150 km range missile it isn't exactly a short-range missile. The range just looks less impressive, compared to the other missiles.

What the M-1 lacks in range is made up for with unit cost. This is especially true as stealthy armed wingman drones comes to the scene. The other missiles are too heavy to be fired from a wingman drone. Deploying a M-1 missile from a wingman will always cost less than deploying a M-2 or M-3 from a heavy fighter.
As we know, these Rudram missiles are for dual purposes as ARM roles or air-to-ground roles, so for Rudram 1 with 100 km as ARM, it should be good for the IAF, IMO.
 
Are we going to induct the RudraM-I?
Rudram 1 is likely de-linked from the program and after NGARM designation comes under DRDL ASL&V group that handle all the astra etc. Deliverable based R2 R3 all are being done by RCI. There must be some reason, esp with TD mentioned in project. Warhead trials was mentioned in 2024 July NL , so probably IAF will take a call. Since ADANI def got it, most likely some order will be done.

Real range of NGARM is 200 kms, maybe even more than that as we always understate our missile's range.
NGARM can do speed/thrust variation , top speed 2 mach close it would obviously lose range hence close to 100-120km max launch range in a quick reaction mode where pilot has locked onto target signature. Otherwise in seek and destroy role, the missile can not move fast like at mach 2 and seek the target signature in the general area hence speed drops to 0.8 mach level aka range increases to almost 200km obviously to seek the target over large terrain. Since target can remain hidden behind valley/hills, going at 2 mach over it and then turning back is not possible so a lower speed is ideal in this mode.
 
Interestingly, though Rudram III is an air-launched missile, it uses a booster phase and a separation technique, so in the terminal phase, the tail fin section is going to be separated. The design seems to be pretty complex for an ARM design and IMO it might be intended for use against aerial targets.
Its not for seek and destroy role, ie typical sead mission in a contested battlefield perhaps. That role requires covering a large sector at a slower speed so the seeker system can pick up the target at a smaller range compared to when the carrier aircraft got the radar lock on the target radar and launched it afterwards. In fact the poster before showed radar installation ie a large fixed target object.

Given that level of standoff distance to be covered, and likely in the speed/kinetic impulse regime that is planned for R2 , obviously it needed both dual pulse config and a booster. What we have learned from the general literature based knowledge so far, almost certainly it will be able to hit something at 600km away within 7-8 mins of launch, probably for less time.

To hit aerial maneuvering target, it will prob need some modification in airframe and a different programmed obc.
 
Its not for seek and destroy role, ie typical sead mission in a contested battlefield perhaps. That role requires covering a large sector at a slower speed so the seeker system can pick up the target at a smaller range compared to when the carrier aircraft got the radar lock on the target radar and launched it afterwards. In fact the poster before showed radar installation ie a large fixed target object.

Given that level of standoff distance to be covered, and likely in the speed/kinetic impulse regime that is planned for R2 , obviously it needed both dual pulse config and a booster. What we have learned from the general literature based knowledge so far, almost certainly it will be able to hit something at 600km away within 7-8 mins of launch, probably for less time.

To hit aerial maneuvering target, it will prob need some modification in airframe and a different programmed obc.
So its for "fixed" installations?
In that case it probably wouldn't need a AR seeker
So isn't it a precision ground strike missile, rather than a arm missile, like you can hit fixed radar installations with brahmos or any other precision missile.
 
Interestingly, though Rudram III is an air-launched missile, it uses a booster phase and a separation technique, so in the terminal phase, the tail fin section is going to be separated. The design seems to be pretty complex for an ARM design and IMO it might be intended for use against aerial targets.

View attachment 45679View attachment 45683
Rudram-3 is a hypersonic ALBM in the same class as ROCKS/Blue Sparrow. ROCKS reportedly also has an optional passive seeker.

The massive tail control surfaces are likely for maneuverability immediately after launch.
 
So its for "fixed" installations?
In that case it probably wouldn't need a AR seeker
So isn't it a precision ground strike missile, rather than a arm missile, like you can hit fixed radar installations with brahmos or any other precision missile.
What is AR seeker ? its usually rf, phh type seekers. IIR seeker will aid in precision targeting beating any countermeasure (smokescreen etc).
fixed installation does not mean its a small footprint on the ground. Think of a big dome on a remote site and within that site the dome sits somewhere. So a computer would not know unless it fed signal analyse and algo determine its a radar signal emitting object and locks onto that position. Hence missile need the seeker for precision targeting.
As per the poster shown in Hyderabad, its also dual purpose. Of course anything can hit a radr installation, but compared to R3 class missile a brahmos will take 10min+ to get to the target and its a deep penetration kind of missile with high terminal velocity. In comparison R3 also retain good impact velocity but does not need to penetrate few meters of concrete or take 10+ mins to reach the target so enemy reaction time is less. Both missiles are good enough to evade and stay below that radars tracking horizon.
Rudram-3 is a hypersonic ALBM in the same class as ROCKS/Blue Sparrow. ROCKS reportedly also has an optional passive seeker.

The massive tail control surfaces are likely for maneuverability immediately after launch.
Do not know if its rocks or the other israeli air launched stuff, but read in their site that the missile after launch takes a ballistic trajectory. None of our missiles ever follow a ballistic trajectory hence these are so much computation exhaustive (and takes time to be perfect).
 
Rudram 2 Brochure from Defence Expo 2022
View attachment 44430

Common features:
Propulsion : Solid Rocket Motor
Navigation : INS + SATNAV
Actuation : EMA
Range : 50-300 Km
Launch Platform : Su 30MKI & Mirage 2000
Launch Mach : 0.5 to 1.5
Launch Alt : 3 to 15 Km
Apogee : 40 km
Time of Flight : 400sec
Mach number : Peak (5.5) Touchdown (>1.0)
WH Weight : 200 Kg class
Control : Aerodynamic


ARM Role
Seeker : PHH+IIR
Warhead : PF-155 Kg
Impact Angle : 40°-50°
Target : Radar Installations

Ground Attack Role
Seeker : IIR
Warhead : PCB-200 Kg
Impact Angle : 80°
Target : Bunkers, Air Strips, Hangars


Rudram 2 Brochure from Vigyan Vaibhav 2025
View attachment 44431

Specifications
Range : 50 - 300 km
Diameter : 455 mm
Length : 4995 mm
Mass : 1025 kg
Propulsion : Solid Rocket Motor
Navigation : INS + SATNAV
Actuation : EMA
Launch Platform : Su 30MKI
Launch Mach : 0.5 to 0.9
Launch Alt : 3 to 11 Km
Apogee : 40 km
Time of Flight : 300sec
Mach number : Peak (5.5) Touchdown (>1.0)
WH Weight : 200 Kg class
Control : Aerodynamic

Ground Attack Role
Seeker : IIR
Warhead : PCB-200 Kg
Impact Angle : 80°
Target : Bunkers, Air Strips, Hangars

ARM Role
Seeker : RF seeker
Warhead : PF-155 Kg
Impact Angle : 40°-50°
Target : Radar Installations

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Rudram 3

Brochure from Vigyan Vaibhav 2025
View attachment 44432


Rudram 3 Brochure from Defence Expo 2022
View attachment 44433

RudraM- 3 is an Air to Surface missile capable of neutralizing Radiating targets and ground targets including Bunkers, Buildings, Shelters at long ranges.

SALIENT FEATURES
Capable to be launched trom Su-30mki
Passive and Active dual mode seeker
Possible lock on before launch
Highly manoeuvrable missile
All weather Day and night capability
All thorough supersonic

CURRENT STATUS
Under Devlopment

LAB
Research Centre Imarat Hyderabad as Nodal Lab


Unknown Origin Schematics of Rudram 3 (possibly for a scale model)
View attachment 44434
View attachment 44435

Projected Specifications (My guestimates)
Range : 500- 550 km
Diameter : 560 mm
Length : 6000 mm
Mass : 1.6 -1.8 ton
Propulsion : 2 Stage Solid Rocket Motor
Navigation : INS + SATNAV
Actuation : EMA
Launch Platform : Su 30MKI
Launch Mach : ?
Launch Alt : ?
Apogee : ?
Time of Flight : ?
Mach number : ?
WH Weight : 150 Kg class (125 kg PCB warhead)
Control : Aerodynamic
A slide on Rudram 3 from Aero India 2025
1758065872241.jpeg
Mass of the Missile Confirmed to be >1500 kg

Challenges w.r.t integration of RudraM
• First time a weapon weighing more than 1500 kg and 6 m long successfully flown with two missiles suspended from Stn 5&6.
• Weapon integrity proven in its captive envelop.
• Modified launcher and LPSU were proved for entire captive envelope
• Max strains observed are within eye lugs load capability
• Weapon integrity proven for Supersonic sp
• Aircraft found safe from flutter point of its combat mode
 
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