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Answer: 2027-28
Chandrayaan-4 aims to collect ~2-3 kg lunar regolith from south pole region and return to Earth; complex multi-module mission targeting late 2020s window.
Answer: Orbit-to-surface/orbit
Rotating tether catches/releases payloads at periapsis/apoapsis transferring orbital energy; enables access to LEO/GEO/lunar surface without rockets.
Answer: 120
Three DSN sites (Goldstone/Madrid/Canberra) at ~120° spacing ensure at least one complex maintains link with deep space probes as Earth rotates.
Answer: Crystal formation
Student payloads on POEM leverage spent PS4 stage for affordable microgravity research; crystal growth experiments inform pharmaceutical/materials science.
Answer: toxicity/handling hazards
Hydroxylammonium nitrate-based propellants eliminate carcinogenic hydrazine handling risks while delivering ~10% higher Isp; adopted in GPIM/ESCAPADE missions.
Answer: cost and mass
Micro-electromechanical systems gyros offer adequate performance for CubeSat/nanosat ADCS at fraction of FOG cost/mass; commercial availability enables proliferation.
Answer: NETRA/ISTRAC
ISSAR documents space object cataloguing, conjunction assessments, and debris environment trends; released by ISRO SSA control centre.
Answer: Mirrors
Nickel electroformed mirror shells replicated from mandrels enable nested Wolter-I optics for focusing grazing-incidence X-rays; used in XMM-Newton/eROSITA.
Answer: 150
GEO disposal requires raising perigee ≥300 km above GEO belt (~150 m/s ΔV) to prevent collision risk; mandated by IADC guidelines.
Answer: HSFC
Human Space Flight Centre (HSFC) Bengaluru manages astronaut selection/training, crew systems, and mission integration for Gaganyaan.
Answer: Lunar Gateway
Canadarm3 provides autonomous external robotics for Gateway assembly/maintenance; features AI-enhanced dexterity for uncrewed operations in cislunar space.
Answer: Heavy/large-volume
Deployable/inflatable heat shields enable delivery of massive payloads to Mars/Venus where rigid aeroshells are volume/mass constrained; tested in LOFTID/IRVE missions.
Answer: Thiruvananthapuram
SPL at VSSC Thiruvananthapuram studies ionosphere/thermosphere using ground-based instruments and satellite data, supporting space weather forecasting.
Answer: stiffness-to-weight
Aluminum/Nomex honeycomb cores bonded to face sheets provide exceptional bending stiffness at minimal mass, ideal for satellite bus and payload panels.
Answer: Bengaluru
ISTRAC HQ in Bengaluru coordinates global network of ground stations supporting LEO/GEO/deep space missions with real-time TT&C services.
Answer: Staged combustion
SCE-200 employs oxygen-rich staged combustion cycle burning kerosene/LOX, delivering 200-ton thrust class performance for future heavy-lift vehicles.
Answer: stronger and defect-free
FSW solid-state process avoids melting/solidification defects, yielding superior mechanical properties for cryogenic tank structures in PSLV/GSLV/LVM3.
Answer: Hanle
NLST at Hanle (4500 m altitude) will be world's largest off-axis solar telescope (2 m aperture), studying solar magnetic fields and transient phenomena.
Answer: GSLV-F14
GSLV-F14 successfully deployed INSAT-3DS on Feb 17, 2024, enhancing weather forecasting and disaster warning capabilities over Indian Ocean Region.
Answer: 13
IADC comprises 13 national/international space agencies coordinating debris mitigation standards; ISRO joined in 2000s contributing tracking data.