Please note the following corrections required in SOLID PROPELLANT ROCKET MOTOR DESIGN AND TESTING

1. Page 20       "From equation (3.1)," should state "From equations (3.1) and (3.10),"

2. Page 25       "using equations (3.21), (3.19), (3.1)," should state "using equations (3.21), (3.19), (3.4),"

3. Page 27     

4. Page C-2     

5. Page D-2     The pressure thrust term (Pe - Pa) Ae should be added to the expression for thrust (F).