Landing Payloads on Mars
Landing heavy exploratory vehicles on Mars poses unique engineering challenges due to the planet's tenuous atmosphere. The air density is thick enough to generate extreme friction during entry, requiring thermal shielding, yet too sparse to decelerate heavy landers sufficiently using standard parachutes alone. Consequently, mission planners must employ complex hybrid landing architectures. Supersonic parachutes deploy to reduce initial velocities, followed by the ignition of retro-rockets during the final descent phase. For the heaviest rovers, tethered sky-crane systems have been devised to lower vehicles directly onto their wheels, avoiding the hazard of rocket plumes churning up abrasive surface grit.
What can be inferred about Mars's atmosphere regarding spacecraft landings?
- AIt is dense enough to eliminate the danger of surface dust disturbing delicate sensors.
- BIt causes landing modules to require heavier thermal shielding than on any other planet.
- CIt creates friction without offering enough drag for a purely parachute-based landing.
- DIt requires retro-rockets because parachutes fail to deploy in supersonic conditions.