Consider the following statements regarding 'Jwala-MK1', recently seen in the news -
- It is a short-range surface-to-air missile developed by a private Indian start-up.
- It is primarily designed to intercept and destroy hostile unmanned aerial vehicles (UAVs).
- It employs a solid-fuel dual-pulse rocket motor to enable rapid acceleration at launch and extra speed during the final attack phase.
- It has already been fully integrated with a command-and-control battle-management architecture and has completed all system-level flight trials.
How many of the statements given above are correct?
Explanation - Statement 1 is Correct: Jwala-MK1 is a cost-effective short-range surface-to-air missile developed by IG Defence, an Odisha-based private start-up.
Statement 2 is Correct: It is primarily designed to destroy hostile unmanned aerial vehicles (UAVs), unlike conventional air-defence missiles aimed at aircraft or high-value targets.
Statement 3 is Correct: It uses a solid-fuel dual-pulse rocket motor, which enables rapid acceleration at launch and extra speed during the final attack.
Statement 4 is Incorrect: Full propulsion-system integration is still a key step to be achieved (only two solid rocket motors have been test-fired recently). Furthermore, complete-system flight trials, guidance and control validation, and integration with command-and-control architecture are next steps, meaning they have not yet been completed. Therefore, claiming it is "fully integrated" and has "completed all system-level flight trials" is factually wrong.
Explanation - Statement 1 is Correct: Jwala-MK1 is a cost-effective short-range surface-to-air missile developed by IG Defence, an Odisha-based private start-up.
Statement 2 is Correct: It is primarily designed to destroy hostile unmanned aerial vehicles (UAVs), unlike conventional air-defence missiles aimed at aircraft or high-value targets.
Statement 3 is Correct: It uses a solid-fuel dual-pulse rocket motor, which enables rapid acceleration at launch and extra speed during the final attack.
Statement 4 is Incorrect: Full propulsion-system integration is still a key step to be achieved (only two solid rocket motors have been test-fired recently). Furthermore, complete-system flight trials, guidance and control validation, and integration with command-and-control architecture are next steps, meaning they have not yet been completed. Therefore, claiming it is "fully integrated" and has "completed all system-level flight trials" is factually wrong.