y1=−m(2×k)×In((T−mg−kv2)(T−mg))
Use this algorithm to calculate how many Newtons of force a rocket gives off.
m = mass of rocket
g = 9.81 m/s²
v = velocity of rocket
y = height rocket reaches
k = wind resistance forces
T = motor thrust in Newtons (AKA what we're solving for.)
y1=−m(2×k)×In((T−mg−kv2)(T−mg))
Use this algorithm to calculate how many Newtons of force a rocket gives off.
m = mass of rocket
g = 9.81 m/s²
v = velocity of rocket
y = height rocket reaches
k = wind resistance forces
T = motor thrust in Newtons (AKA what we're solving for.)
T=?
y1=−m2k⋅ln(T−(mg+kv2)T−mg)−2y1km=ln(T−(mg+kv2)T−mg)|exe−2y1km=T−(mg+kv2)T−mg1e2y1km=T−(mg+kv2)T−mge2y1km=T−mgT−(mg+kv2)[T−(mg+kv2)](e2y1km)=T−mgT⋅(e2y1km)−(mg+kv2)⋅(e2y1km)=T−mgT⋅(e2y1km−1)=(mg+kv2)⋅(e2y1km)−mgT=(mg+kv2)⋅(e2y1km)−mg(e2y1km−1)
y1=−m(2×k)×In((T−mg−kv2)(T−mg))
Use this algorithm to calculate how many Newtons of force a rocket gives off.
m = mass of rocket
g = 9.81 m/s²
v = velocity of rocket
y = height rocket reaches
k = wind resistance forces
T = motor thrust in Newtons (AKA what we're solving for.)
T=?
y1=−m2k⋅ln(T−(mg+kv2)T−mg)−2y1km=ln(T−(mg+kv2)T−mg)|exe−2y1km=T−(mg+kv2)T−mg1e2y1km=T−(mg+kv2)T−mge2y1km=T−mgT−(mg+kv2)[T−(mg+kv2)](e2y1km)=T−mgT⋅(e2y1km)−(mg+kv2)⋅(e2y1km)=T−mgT⋅(e2y1km−1)=(mg+kv2)⋅(e2y1km)−mgT=(mg+kv2)⋅(e2y1km)−mg(e2y1km−1)