Why do hypersonic vehicles lose radio contact during reentry?
The air around the vehicle ionizes into a plasma sheath that absorbs and reflects radio waves, causing the 'communications blackout' until it slows and the plasma thins out.
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The air around the vehicle ionizes into a plasma sheath that absorbs and reflects radio waves, causing the 'communications blackout' until it slows and the plasma thins out.
A ballistic missile follows a predictable arcing path set at launch, while a hypersonic glide vehicle stays in the atmosphere and maneuvers, making its trajectory far harder to predict.
It pushes against its own exhaust: by Newton's third law, throwing mass backward at high speed produces an equal forward thrust, no external medium needed.
Think of a skateboarder throwing heavy bricks — each brick hurled one way shoves them the other. A rocket just throws very hot, very fast 'bricks' of exhaust.
Orbit means falling around the Earth fast enough to keep missing it, so you need roughly 7.8 km/s sideways velocity; most of a rocket's energy goes into speed, not height.
Mostly compression of the air piling up in front of the vehicle, not friction; it heats to thousands of degrees and heat shields ablate or radiate that energy away.
Surfaces can reach up to around 1,650°C (3,000°F) for capsules, and far hotter for high-speed lunar returns, as the compressed air dumps its energy into the vehicle.
A blunt shape pushes a detached shock wave ahead of the vehicle, keeping most of the searing heat in the air rather than in the structure.
Specific impulse measures how much thrust you get per unit of propellant burned; higher values mean more delta-v from the same mass of fuel.
Dropping empty tanks mid-flight sheds dead weight, so the remaining engines accelerate a lighter vehicle and beat the exponential fuel cost of the rocket equation.
They use aerodynamic control surfaces and body lift, sometimes with reaction-control thrusters, shifting the lift vector to pull turns the atmosphere alone could not.
Tsiolkovsky's equation links delta-v to exhaust velocity and mass ratio; because it's exponential, small velocity gains demand disproportionately huge increases in fuel.
A scramjet burns fuel in supersonic airflow, like keeping a flame lit in a hurricane, with only milliseconds for the air to mix and combust.
They fuse radar and satellite tracks with a physics model of the vehicle's dynamics and estimate its likely intent, producing a probability corridor rather than a single point.
Even the thin upper atmosphere creates drag that slowly saps their speed, lowering the orbit until it decays and the satellite reenters.
Above about Mach 5 the shock waves hug the body, the air chemically dissociates, and heating dominates the design, so supersonic models stop being accurate.
Delta-v is the total change in velocity a spacecraft can achieve; every maneuver spends some, so it's the fundamental budget for any mission.
The roughly 100 km altitude often used as the edge of space, where the air is too thin for wings to generate lift and you'd need orbital speed instead.
To borrow the Earth's rotational speed (about 1,670 km/h at the equator), giving a free head start toward orbital velocity.
Liquid engines can be throttled and shut down but are complex, while solid motors are simple and powerful but burn until exhausted once lit.
Ablative shields char and slough away, carrying heat off with the lost material, while reusable tiles insulate and radiate the heat back out.
A spacecraft borrows a tiny bit of a planet's orbital momentum during a close flyby to gain speed without burning fuel.
Space is nearly empty, so there's almost nothing to carry heat away; a craft can only shed heat by radiating it, so its sunlit side can bake.
In an elliptical orbit, apogee is the farthest point from Earth and perigee the closest; a craft moves slowest at apogee and fastest at perigee.
They carry atomic clocks and even correct for relativity — time runs slightly faster for them in weaker gravity — keeping positioning within meters.
Roughly 6,100 km/h at sea level; past Mach 5 the heating and air chemistry shift enough that engineers treat it as a separate flight regime.
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