Ch 2: The S/C Environment and its Effect on Design 1/2 Flashcards
Main sources of noise and vibration during launch
- LV engines
- aerodynamic buffeting in lower atmosphere
aerodynamic buffeting
Buffeting is a high-frequency instability, caused by airflow separation or shock wave oscillations from one object striking another. It is caused by a sudden impulse of load increasing. It is a random forced vibration.
Peak vibration/acoustic levels during launch
- LIFT-OFF: rocket motor + ground reflection of exhaust products -> primary vibration to PL through structural elements and secondary through the launch shroud
- TRANSONIC FLIGHT
peak acceleration depending on LV
HIGH PEAK ACC - low-mass LVs (obvs), air-launched
multistage - peak at seperation
what is the thermal environment during launch determined by?
launch shroud temperature
after ejection - friction, but by then low atmospheric density
determining the temperature reached during launch
specific heat of the shroud material
friction heating vs radiative + convective heat loss
depressurisation rate
venting ports in shrouds
venting ports esp. required where in PL?
electronic boxes
EMI
EM interference; huge hazard during launch
-> PL prop ignition etc
Sun mass
~2e30 kg
Sun radiated light peak λ
~460 nm
Interstellar gas density
~3 atoms/cm^3
Sun surface temperature
~5800 K
Sun radiation - regions causing dips from the BB curve
CHROMOSPHERE: lower atmosphere, few thousand kms above the photosphere, increasing temperature to ~10e3 K -> enhanced UV emission
CORONA: upper atmosphere, extends to a few solar radii, 2e6 K -> X-rays emission
solar wind - what, where from, physical properties @ Earth
flow of plasma expelled at high velocity; outermost layer of solar atmosphere
@ Earth: ~450 km/s, ~9 protons/cm^3, kinetic temp ~100e3 K