-L
L..
1.3. 3
The
Location of Center of Gravity with Tolerance
spacecraft center of gravity coordinates above the separation plane are as follows:
NXX
X
=
=
872.1 + 2.5 mm
+ (34.3 0.1 in.)
0.4 + 2.5 mm (0.02 0.1 in.)
Y = 0.2 + 2.5 mm
1.3.4
(0.01 0.1 in.)
Description of Sloshing Fluid Masses
shape;
There are four diametrically opposed reaction system (RCS) fuel tanks of conispherical contains 52.8 kg (116.4 pounds) of hydrazine.
1.3.5
Dynamic Balance with Tolerances
IZX = 0.95 + 0.14 kg-m2 (0.7+ 0.1 slug-ft2) IZY = 0.40 + 0.14 kg-m2 (0.29 ± 0.1 slug-ft2) IXY = 12.74 + 1.4 kg-m2 (9.37 +1.0 slug-ft2)
1.4 Launch Day
control each
As
specified
in Article
6 of the Launch
Services
Contract.
1.5
Launch Windows
The Client's Spacecraft is required to have at one launch window within each day of the launch period. Each launch window should be no less than 45 min. If the
Client, the above requirement is not suitable to the Client shall present his special requirement to for this purpose. The specific launch satisfy spacecraft constraints are TBD.
least
CGWIC
windows
which
2.
MAIN INTERFACES
2.1
ANNEX I
Mechanical Interfaces
2.1.1
The
Spacecraft Mounting
Spacecraft will be mated to the 37
inch adaptor
with a clampband provided by CGWIC, and then integrated with the LM-3. Further, a separation system with inside arrangement of four separation springs and microswitches mounted on the Launch Vehicle provided by CGWIC.
the two will
be
3