Apollo 15 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

223:48:45.84

67.6

5,305.9

 

 

0.52

-128.90

Transearth injection cutoff

223:51:06.74

71.8

8,272.4

140.90

3,046.8

4.43

-129.08

Midcourse correction ignition

291:56:49.91

25,190.3

11,994.6

 

 

-68.47

103.11

Midcourse correction cutoff

291:57:12.21

25,149.3

12,002.4

22.30

5.6

-68.49

103.09

CM/SM separation

294:43:55.2

1,951.8

29,001.7

 

 

-36.44

56.65

 

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