HLV - Heavy-lift Launch Vehicle от ISRO

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http://www.b14643.de/Spacerockets_1/India/ULV/Description/Frame.htm

HLV

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.

Canceled HLV

http://www.b14643.de/Spacerockets_1/India/LVM3/Versions/LVM3.htm

LVM3, ULV, HLV & SHLV

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)