http://www.b14643.de/Spacerockets_1/India/ULV/Description/Frame.htm
Цитата: undefinedHLV
A Heavy lift Launch Vehicle capable of placing up to 10 ton class of spacecrafts into Geosynchronous Transfer Orbit is currently under study by a project team. This new generation launch vehicle will derive its propulsion modules from LVM3 as well as from new developments, which include :
- Larger S-250 solid strap on boosters as compared to S-200 strap on motors used in LVM3
- Larger L-200 semi cryogenic booster stage, SCE-200 engine
- Larger cryogenic upper stage (L-100) with CE-60 engine.
This HLV concept (one SCE-200 engine and a cryogenic CE-60 engine) is obviously no longer favored. In a new concept, five SCE-200 engines are planned (see Versions, Propulsion).
SHLV
A future SHLV concept with liquid-fuel boosters and 5 engines SCE-200 is presented (see Versions, Propulsion). The payload capability is 16.3 t for GTO and 41.3 t for LEO. A version without booster should have a capability of 4.9 t for GTO and 11.4 t for LEO.
(https://img.novosti-kosmonavtiki.ru/223536.jpg)(https://img.novosti-kosmonavtiki.ru/223535.jpg)
Canceled HLV
http://www.b14643.de/Spacerockets_1/India/LVM3/Versions/LVM3.htm
Цитата: undefinedLVM3, ULV, HLV & SHLV |
(https://img.novosti-kosmonavtiki.ru/223534.jpg)
| Version | Booster | Stage 1 | Stage2 | | LVM3 D1, D2 | (GSLV-Mk3) | 2 x S-200 | L-116 (UDMH/N2O4) | HTVE SL (2 | L-28 (LH2/LOX) | CE-20 | | LVM3 DX | HPVE-1 (2) | | ULV | Light | | 6 x S-13 (PSOM-XL) | L-160 (Kerosene/LOX) | SCE-200 | L-35 (LH2/LOX) | CE-20 | | Heavy | | 2 x S-200 | L-160 (Kerosene/LOX) | SCE-200 | L-35 (LH2/LOX) | CE-20 | | HLV (canceled) | | 2 x S-250 | L-200 (Kerosene/LOX) | SCE-200 | L-100 (LH2/LOX) | CE-60 | | HLV | | 2 x S-250 | L-400 (Kerosene/LOX) | SCE-200 (5) | L-27 (LH2/LOX) | CE-20 | | SHLV | Light | | - | L-500 (?) (Kerosene/LOX) | SCE-200 (5) | L-60 (LH2/LOX) | CE-20 (2) | | Heavy | | 2 x SC-500 ? (5 SCE-200) | L-500 (?) (Kerosene/LOX) | SCE-200 (5) | L-60 (LH2/LOX) | CE-20 (2) |
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