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Intermediate – requires precise knowledge of mission timelines, launch vehicles, payloads, and outcomes; questions often mix technical and programmatic details.
Trap: GSLV uses only indigenous cryogenic engine in all variants – Fact: GSLV Mk I and Mk II used Russian-supplied cryogenic stages initially; indigenous CUS was first successfully flight-tested in GSLV-D5 (2014); LVM3 uses indigenized C25 stage.
Trap: Chandrayaan-2’s lander Vikram successfully landed on Moon – Fact: Vikram attempted landing on September 7, 2019 but deviated during final descent and crash-landed; communication lost at 2.1 km altitude (ISRO Failure Analysis Report, 2019).
Trap: PSLV can launch satellites into geostationary orbit – Fact: PSLV is optimized for polar and low Earth orbits; maximum payload to GTO is ~1.4 tonnes; GSLV/LVM3 required for full geostationary insertion.
Trap: Gaganyaan will launch from Sriharikota using PSLV – Fact: Gaganyaan missions will use LVM3 (GSLV Mk III), the only ISRO vehicle human-rated for crewed launch; launch site is Second Launch Pad, SHAR.
Question: Consider the following statements about Chandrayaan-3: 1. It was launched using the LVM3 launch vehicle. 2. The propulsion module remained in lunar orbit after lander separation. 3. It achieved the first soft landing in the Moon’s equatorial region. Which of the statements given above is/are correct? A) 1 only B) 1 and 2 only C) 2 and 3 only D) 1, 2 and 3 Answer: A Explanation: Statement 1 is correct – Chandrayaan-3 was launched by LVM3 on July 14, 2023. Statement 2 is incorrect – the propulsion module returned to Earth orbit after mission completion. Statement 3 is incorrect – landing was near the south pole (~70°S), not equatorial. Why others fail: Option B is tempting due to partial correctness of 1 and 2, but propulsion module did not stay in lunar orbit.
Question: Which of the following ISRO missions was primarily designed to study solar coronal mass ejections? A) Aditya-L1 B) AstroSat C) XPoSat D) Mangalyaan Answer: A Explanation: Aditya-L1 carries the Visible Emission Line Coronagraph (VELC) to study solar corona and coronal mass ejections from Sun-Earth L1 point. Why others fail: AstroSat observes multi-wavelength astronomy but not solar-specific; XPoSat studies X-ray polarization; Mangalyaan is Mars-focused.
Question: The first Indian mission to use an indigenously developed cryogenic upper stage successfully was: A) GSLV-D3 B) GSLV-D5 C) GSLV-F06 D) LVM3-M1 Answer: B Explanation: GSLV-D5, launched on January 5, 2014, successfully used the indigenous cryogenic upper stage (CUS), placing GSAT-14 into GTO. Why others fail: GSLV-D3 (2010) failed due to CUS ignition failure; GSLV-F06 (2010) used Russian stage; LVM3-M1 (2017) used improved C25 stage but not the first.
Question: Which of the following pairs is correctly matched? 1. NISAR – ISRO-NASA joint mission 2. SpaDeX – Reusable Launch Vehicle experiment 3. Vyommitra – Crew escape system A) 1 only B) 1 and 2 only C) 2 and 3 only D) 1, 2 and 3 Answer: A Explanation: NISAR is a joint mission between ISRO and NASA; SpaDeX is for space docking, not RLV; Vyommitra is a humanoid, not part of escape system. Why others fail: Option D is tempting due to high-profile nature of all terms, but only 1 is correct.
Question: The primary objective of the XPoSat mission is to: A) Map lunar surface composition B) Study X-ray polarization from celestial sources C) Monitor Earth’s ionosphere D) Detect gravitational waves Answer: B Explanation: XPoSat, launched in 2024, carries POLIX and XSPECT to measure polarization of X-rays from black holes, neutron stars, and pulsars. Why others fail: Chandrayaan missions map Moon; Ionosphere monitored by other satellites like INSAT-3DS; gravitational waves not detectable by XPoSat.
Question: Which launch vehicle was used for India’s first successful interplanetary mission? A) PSLV-C25 B) GSLV Mk II C) LVM3-M1 D) PSLV-XL Answer: A Explanation: Mars Orbiter Mission (Mangalyaan) was launched on November 5, 2013, using PSLV-C25 from Sriharikota. Why others fail: GSLV Mk II and LVM3 used for heavier payloads; PSLV-XL is a variant but C25 was the specific vehicle.
Question: Consider the following: 1. CARE module 2. Vyommitra 3. SHAPE payload Which of the above were part of the Chandrayaan-3 mission? A) 1 and 2 only B) 2 and 3 only C) 3 only D) 1, 2 and 3 Answer: C Explanation: SHAPE payload was on the propulsion module of Chandrayaan-3; CARE was part of 2014 LVM3 test; Vyommitra is for Gaganyaan. Why others fail: Option B is tempting due to association with ISRO humanoids and experiments, but Vyommitra not on Chandrayaan-3.
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