Apollo 10 Transearth Phase

 

 

 

 

 

 

Event

 

 

 

 

GET

(hhh:mm:ss)

 

 

 

 

Altitude

(n mi)

 

 

Space

Fixed

Velocity

(ft/sec)

 

 

 

Event

Duration

(sec)

 

 

 

Velocity

Change

(ft/sec)

Space

Fixed

Flight

Path

Angle

(deg)

 

Space

Fixed

Heading

Angle

(E of N)

Transearth injection ignition

137:36:28.9

56.0

5,362.7

 

 

-0.44

-73.60

Transearth injection cutoff

137:39:13.7

56.5

8,987.2

164.8

3,680.3

2.53

-76.68

Midcourse correction ignition

188:49:58.0

25,570.4

12,540.0

 

 

-69.65

119.34

Midcourse correction cutoff

188:50:04.7

25,557.4

12,543.5

6.7

2.2

-69.64

119.34

 

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