07.11.2014 Views

MISSION PLAN - PDS Small Bodies Node

MISSION PLAN - PDS Small Bodies Node

MISSION PLAN - PDS Small Bodies Node

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

Launch<br />

Initial Acquisition<br />

TCM-1<br />

Activation and Checkout<br />

0 - 30<br />

0 - 1<br />

15<br />

1 - 30<br />

30<br />

1<br />

-<br />

29<br />

3.2 Initial Acquisition Subphase<br />

The initial acquisition subphase includes all activities from launch vehicle liftoff to<br />

completion of Deep Space Network (DSN) acquisition. Although one complete day is<br />

allocated for this activity, selection of the short coast launch option allows these activities<br />

to be completed within three hours of launch.<br />

Prior to liftoff (L/O), the spacecraft is powered on via launch vehicle umbilical power at<br />

L/O-240 minutes. The spacecraft is transferred to internal battery power at L/O-4<br />

minutes. At this time the spacecraft is electrically configured for initial cruise mode with<br />

the exception that solar panels are not deployed and the solid-state power amplifier<br />

(SSPA) is off.<br />

The activities from liftoff to spacecraft separation are summarized in Table 3.2-1 and<br />

illustrated in Figure 3.2-1. It should be noted that the numbers presented are specific to a<br />

February 6 launch date, but are typical of other launch dates. However, the specific<br />

numbers are provided for illustrative purposes only and are subject to change as mission<br />

plans mature.<br />

Table 3.2-1 Injection Activities<br />

Event L/O+(sec) (min) Comments<br />

PRE-LAUNCH<br />

1 Spacecraft power ON -86400.0 -1440.0 Latch Valves Closed & System<br />

Wet; EPS, C&DH, Rcvr, & DST<br />

powered<br />

2 Switch to internal power –240.0 -4.0 On batteries<br />

3 Liftoff 0.0 0.0<br />

PRE-SEPARATION<br />

4 Power on Prop Heaters 241.0 4.0 1 lb thrusters, valve, line, tank<br />

5 Main engine cutoff (MECO) 264.0 4.4<br />

6 Stage II ignition 277.7 4.6<br />

7 9.5 ft fairing separation 284.0 4.8<br />

8 First Stage II cutoff (SECO 1) 597.3 10.0<br />

9 Enter Solar Eclipse 902.0 15.0 02/06/99 launch<br />

10 Restart Stage II 1309.8 21.8<br />

11 SECO 2 1414.0 23.6<br />

12 Stage II separation 1467.0 24.5<br />

13 Power on IMU 1485.0 24.8 sep - 2 min, earliest across LP<br />

14 Stage III ignition 1504.0 25.1<br />

15 Stage III burnout 1569.3 26.2<br />

16 Spacecraft separation 1639.0 27.3 Assumes 69.7 seconds coast<br />

17 Open Latch Valves 1640.0 27.3 sep + 1 sec<br />

18 Deploy LV Stage III Yo 1642.0 27.4<br />

DESPIN<br />

46

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!