Question

Difficulty: HardDefense Affairs, Joint Military Exercises, and National Security

Consider the following statements regarding the indigenous Very Short Range Air Defence System (VSHORADS) developed by the Defence Research and Development Organisation (DRDO):

1. It is a Man-Portable Air Defence System (MANPADS) powered by a dual-thrust solid reaction motor.
2. It is designed to neutralize low-altitude aerial threats at short ranges using an unguided radio-frequency command guidance system.
3. The missile system incorporates a miniaturized Reaction Control System (RCS) to ensure high maneuverability during flight.

Which of the statements given above are correct?

  1. 1 and 3 onlyAnswer
  2. B
    2 and 3 only
  3. C
    1 and 2 only
  4. D
    1, 2, and 3

Answer

The correct answer is the option containing statements 1 and 3 only.
Statements 1 and 3 accurately describe the defense technology parameters of VSHORADS: it is a dual-thrust solid motor MANPADS that incorporates a miniaturized Reaction Control System (RCS) for high maneuverability. Statement 2 is false because the weapon system employs an advanced integrated Imaging Infrared (IIR) seeker for target acquisition and homing.

Step-by-Step Solution

1
Evaluate Statement 1 regarding system propulsion and classification.
Statement 1 is correct. VSHORADS is an indigenously developed MANPADS equipped with a dual-thrust solid propellant rocket motor.
DRDO designed the system for rapid deployment against low-altitude threats using solid propulsion.
2
Evaluate Statement 2 regarding guidance technology.
Statement 2 is incorrect. The missile utilizes an integrated Imaging Infrared (IIR) seeker, not an unguided radio-frequency guidance mechanism.
IIR seekers enable high precision against low RCS aerial targets under electronic warfare environments.
3
Evaluate Statement 3 regarding flight maneuvering control.
Statement 3 is correct. The system integrates a miniaturized Reaction Control System (RCS) alongside integrated avionics.
RCS is essential to provide mid-flight stability and sharp terminal maneuverability at close engagement ranges.

Key Concept

DRDO VSHORADS Missile System Parameters & Guidance Architecture
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