kingkong123
Member
- Joined
- Dec 20, 2011
- Messages
- 98
- Gender
- Male
- HSC
- 2012
Hi guys,
I've been revising over a bit of space and have come across questions asking to calculate the size of a rocket's thrust when they give you they velocity of the exhaust gas and the rate a which it burns. Eg. A rocket with an exhaust velocity of 1.3 × 10^3 ms^–1 burns fuel at a rate of 2.7 × 10^3 kg s^–1. What is its thrust? Could someone please provide me with an explanantion of how to approach these questions?
Thanks ay
I've been revising over a bit of space and have come across questions asking to calculate the size of a rocket's thrust when they give you they velocity of the exhaust gas and the rate a which it burns. Eg. A rocket with an exhaust velocity of 1.3 × 10^3 ms^–1 burns fuel at a rate of 2.7 × 10^3 kg s^–1. What is its thrust? Could someone please provide me with an explanantion of how to approach these questions?
Thanks ay