Pages that link to "Item:Q5042930"
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The following pages link to MATHEMATICAL SIMULATION OF A TETHERED SATELLITE SYSTEM MOTION WITH AN INFLATABLE SPHERICAL BALLOON DURING A SPACECRAFT ORBIT INJECTION (Q5042930):
Displaying 3 items.
- Impact of the thermo-mechanical behavior of elastomeric membrane on the flight dynamics of sounding balloons (Q2691065) (← links)
- A way for accelerated calculation of spacecraft motion in an atmosphere with a tethered aerodynamic stabilizer (Q2961180) (← links)
- Anchoring and migration of balloon in REBOA (Q5155050) (← links)